DIADEME 1
Country: French Republic
Live Position
Ground Track · Last 90 Minutes
Upcoming Passes · Over Your Location
About This Satellite
DIADEME 1 is listed as a payload under NORAD ID 2674 with international designator 1967-011A. According to the GCAT master catalog, it was built by National Space Research Center, on the D-1 platform, with a catalog mass of 23 kg, with a shape described as Cyl + 4 Pan. It is associated with French Republic. In the historical build snapshot (TLE epoch 2026-09-05), its LEO orbit had an apogee of about 786 km and a perigee near 502 km, with an inclination of 39.91° and a period of roughly 97.6 minutes; at apogee its speed was about 7.38 km/s. It was launched on 1967-02-08. The build snapshot uses a TLE with epoch 2026-09-05. A moving map, when available, is a prediction rather than a direct measurement.
What this identity tells us
The payload classification comes from GCAT record S02674. A catalog identifier follows a tracked physical object, not necessarily an active service. Manufacturer and owner entries describe catalog associations; ownership is not interchangeable with present-day operation. A separately sourced mission history has not yet been verified for this record.
Reading this orbital snapshot
Based on TLE epoch: 2026-09-05. Estimated altitude ranges from 502 km at perigee to 786 km at apogee, a difference of 284 km. The orbital period is about 97.6 minutes. Eccentricity 0.02024 shows why a single altitude cannot describe the whole path. In a two-body approximation, perigee speed is 1.04 times apogee speed. These are mean-element estimates, not instantaneous measurements. Distance per orbit uses an ellipse approximation.
Saved build snapshot. If a valid TLE is retrieved, this explanation and the orbit panel update together. Otherwise this dated snapshot is retained.
Ground track is not sensor coverage
An inclination of 39.91 degrees implies approximate geocentric ground-track limits of 39.9 degrees north and south. This is a prograde orbit, moving in the same general direction as Earth rotation. The plotted line marks the point beneath the object. It does not represent camera coverage, radio reception, or a guaranteed visible pass.
Accuracy and missing information
The introductory record describes the build snapshot. The orbital snapshot explanation and orbit panel share any successfully retrieved TLE; check the displayed epoch. Reentered objects retain historical data only. Mission history is not rewritten by TLE updates. TLE/SGP4 positions are predictions and can change after maneuvers or updated observations. The 14-day stale-data cutoff is a display safeguard, not an accuracy guarantee. Local passes are geometric predictions, not a visibility forecast. No verified operator or mission status means unknown, not active. Do not use this catalog for collision avoidance or operational flight decisions.
Catalog sources: CelesTrak SATCAT: NORAD 2674 · GCAT: S02674 (source update 2026 Sep 4 2345:57). Supplementary metadata: SatNOGS DB, retrieved 2026-09-05T12:57:25.375Z. Page assembled 2026-09-15. GCAT phase codes describe trajectory phases, not mission health.
Learn more: TLE data · Perigee and apogee · Ground tracks · JOT (Jewawud Live Orbital Map)