TEMISAT, 22783
Orbit data source: Space-Track
TEMISAT, 22783 is a payload satellite owned by Telespazio (IT) in LEO that was launched on Tue, 31 Aug 1993 UTC via a TSIKLON-3 launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). Payload-class satellites include a variety of spacecraft 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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22783 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
Kayser-Threde
Mission
Commercial Communications
Bus & Motor
TEMISAT, Unknown motor
Mass
~42 kg wet, ~42 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Poly, 0.3 m
Radar Cross Section
0.140 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 TEMISAT
1 22783U 93055B 26264.28893279 .00000045 00000-0 27526-4 0 9997
2 22783 82.5508 221.6841 0021645 301.1669 58.7368 13.83900757669001Epoch: 2026-09-21T06:56Z
TLE epoch observation values (Epoch: 2026-09-21T06:56:03.793Z)
Latitude
-0.00005°
Longitude
117.49739°
Altitude
944.777 km
Speed
7.384 km/s
True Right ascension
14h 46m 44s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:53:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
963.091 km
Perigee altitude
931.38 km
Semi-major axis
7,325.373 km
Eccentricity
0.00216
Inclination
82.5508°
RAAN
221.6841°
Arg. of periapsis
301.1669°
True anomaly
58.94911°
Mean anomaly
58.7368°
Eccentric anomaly
58.84293°
Mean motion
3.46177 °/min
Orbital period
103.99 mins
BSTAR
0.000027526
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Other satellites on launch #55 in the year 1993 (1993-08-31 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.TEMISAT Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-09-21 20:56:14.764Z | 134.933° SE | 2026-09-21 21:00:14.764Z | 89.432° E | 25.459° | 2026-09-21 21:05:14.764Z | 33.435° NE |
| 10 mins | 2026-09-21 22:40:14.764Z | 215.153° SW | 2026-09-21 22:45:14.764Z | 288.78° WNW | 44.454° | 2026-09-21 22:50:14.764Z | 352.493° N |
| 7 mins | 2026-09-22 07:50:14.764Z | 36.365° NE | 2026-09-22 07:53:14.764Z | 72.343° E | 20.906° | 2026-09-22 07:57:14.764Z | 114.86° SE |
| 10 mins | 2026-09-22 09:34:14.764Z | 338.515° N | 2026-09-22 09:38:14.764Z | 270.931° WNW | 57.424° | 2026-09-22 09:44:14.764Z | 190.758° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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