SIMSAT 2, 26366
Orbit data source: Space-Track
SIMSAT 2, 26366 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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26366 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 | 660 kg wet, 660 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 2
1 26366U 00026B 25070.91808380 .00004888 00000-0 18589-3 0 9994
2 26366 86.3521 354.6516 0005301 185.5171 174.6018 15.26500395372620Epoch: 2025-03-11T22:02Z
Definitive object data (Epoch: 2025-03-11T22:02:02.44Z)
| Latitude | -0.00003° |
| Longitude | -145.67271° |
| Altitude | 493.087 km |
| Speed | 7.616 km/s |
| True Right ascension | 23h 38m 36s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -85.74165° |
| Longitude | 155.79754° |
| Altitude | 514.865 km |
| Speed | 7.605 km/s |
| Apparent Right ascension | 21h 39m 26s |
| Apparent Declination | -63° 56' 12" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 09:50:59 |
| Azimuth | 176.89° S |
| Elevation | -65.919° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 486.757 km |
| Perigee altitude | 479.483 km |
| Semi-major axis | 6,861.257 km |
| Eccentricity | 0.0005301 |
| Inclination | 86.3521° |
| RAAN | 354.6516° |
| Arg. of periapsis | 185.5171° |
| True anomaly | 174.60751° |
| Mean anomaly | 174.6018° |
| Eccentric anomaly | 174.60466° |
| Mean motion | 3.81889 °/min |
| BSTAR | 0.00018589 |
| Orbital period | 94.27 mins |
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Other satellites on launch #26 in the year 2000 (2000-05-16 UTC)
| SIMSAT 1, 26365 |
| SL-19 R/B, 26367 (Decayed) |
SIMSAT 2 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-03-12 06:27:58.487Z | 25.761° NE | 2025-03-12 06:30:58.487Z | 95.44° ESE | 25.253° | 2025-03-12 06:32:58.487Z | 136.959° SSE |
| 4 mins | 2025-03-12 20:12:58.487Z | 249.898° W | 2025-03-12 20:13:58.487Z | 271.249° WNW | 19.079° | 2025-03-12 20:16:58.487Z | 328.336° NNW |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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