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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Edit Public Description
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, 0.2 m
Radar Cross Section
0.140 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 TEMISAT
1 22783U 93055B 25260.77142107 .00000035 00000-0 18759-4 0 9990
2 22783 82.5536 154.1281 0021529 252.4493 107.4315 13.83871982618032Epoch: 2025-09-17T18:30Z
TLE epoch observation values (Epoch: 2025-09-17T18:30:50.78Z)
Latitude
-0.00001°
Longitude
-120.52607°
Altitude
957.845 km
Speed
7.37 km/s
True Right ascension
10h 16m 30s
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
21:22:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
963.108 km
Perigee altitude
931.566 km
Semi-major axis
7,325.474 km
Eccentricity
0.00215
Inclination
82.5536°
RAAN
154.1281°
Arg. of periapsis
252.4493°
True anomaly
107.66668°
Mean anomaly
107.4315°
Eccentric anomaly
107.54911°
Mean motion
3.4617 °/min
Orbital period
104 mins
BSTAR
0.000018759
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-09-18 05:31:09.809Z | 337.491° NNW | 2025-09-18 05:36:09.809Z | 268.904° W | 35.971° | 2025-09-18 05:41:09.809Z | 200.477° SSW |
| 10 mins | 2025-09-18 17:11:09.809Z | 160.894° S | 2025-09-18 17:16:09.809Z | 82.112° E | 37.349° | 2025-09-18 17:21:09.809Z | 20.16° NNE |
| 7 mins | 2025-09-18 18:58:09.809Z | 252.637° W | 2025-09-18 19:01:09.809Z | 290.918° WNW | 21.818° | 2025-09-18 19:05:09.809Z | 336.213° NNW |
| 9 mins | 2025-09-19 04:05:09.809Z | 17.154° NNE | 2025-09-19 04:09:09.809Z | 78.203° E | 32.297° | 2025-09-19 04:14:09.809Z | 141.661° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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