SIMSAT 1, 26365
Orbit data source: Space-Track
SIMSAT 1, 26365 is a payload satellite owned by Eurockot (CIS) in LEO that was launched on Tue, 16 May 2000 UTC via an ROKOT launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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26365 intel report (Beta)
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Edit Public Description
| Identifier | |
| Orbit | LEO |
| Last TLE update | 7 hours ago |
| Origin | |
| Manufacturer | Khrunichev |
| Mission | Commercial Technology |
| Bus & Motor | SIMSAT, Unknown motor |
| Mass | 657 kg wet, 657 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 1 Arm, 3.5 m |
| Radar Cross Section | 9.625 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 7 hours ago
0 SIMSAT 1
1 26365U 00026A 25071.20273742 .00005060 00000-0 19979-3 0 9991
2 26365 86.3505 358.2962 0006023 292.7178 67.3431 15.25257117372128Epoch: 2025-03-12T04:51Z
Definitive object data (Epoch: 2025-03-12T04:51:56.513Z)
| Latitude | 0.00001° |
| Longitude | 115.21602° |
| Altitude | 491.6 km |
| Speed | 7.62 km/s |
| True Right ascension | 23h 53m 11s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 75.54873° |
| Longitude | 129.32979° |
| Altitude | 506.343 km |
| Speed | 7.616 km/s |
| Apparent Right ascension | 03h 05m 25s |
| Apparent Declination | 22° 26' 19" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 15:50:44 |
| Azimuth | 11.731° NNE |
| Elevation | -26.756° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 490.986 km |
| Perigee altitude | 482.717 km |
| Semi-major axis | 6,864.989 km |
| Eccentricity | 0.0006023 |
| Inclination | 86.3505° |
| RAAN | 358.2962° |
| Arg. of periapsis | 292.7178° |
| True anomaly | 67.40681° |
| Mean anomaly | 67.3431° |
| Eccentric anomaly | 67.37495° |
| Mean motion | 3.81578 °/min |
| BSTAR | 0.00019979 |
| Orbital period | 94.35 mins |
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Other satellites on launch #26 in the year 2000 (2000-05-16 UTC)
| SIMSAT 2, 26366 |
| SL-19 R/B, 26367 (Decayed) |
SIMSAT 1 Visibility forecast
Observer location: undefined°, undefined
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-03-12 19:09:44.755Z | 150.555° SSE | 2025-03-12 19:12:44.755Z | 85.245° E | 29.439° | 2025-03-12 19:15:44.755Z | 23.107° NE |
| 4 mins | 2025-03-13 06:38:44.755Z | 43.806° NE | 2025-03-13 06:39:44.755Z | 70.155° E | 25.878° | 2025-03-13 06:42:44.755Z | 139.636° SSE |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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