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 25359.31833710 .00000063 00000-0 43476-4 0 9991
2 22783 82.5513 75.9313 0022246 339.7999 20.2279 13.83882546631663Epoch: 2025-12-25T07:38Z
TLE epoch observation values (Epoch: 2025-12-25T07:38:24.325Z)
Latitude
0.00004°
Longitude
-132.74514°
Altitude
937.754 km
Speed
7.391 km/s
True Right ascension
05h 03m 43s
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
16:51:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
963.596 km
Perigee altitude
931.004 km
Semi-major axis
7,325.437 km
Eccentricity
0.00222
Inclination
82.5513°
RAAN
75.9313°
Arg. of periapsis
339.7999°
True anomaly
20.31627°
Mean anomaly
20.2279°
Eccentric anomaly
20.27206°
Mean motion
3.46173 °/min
Orbital period
103.99 mins
BSTAR
0.000043476
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Other satellites on launch #55 in the year 1993 (1993-08-31 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-25 18:40:25.939Z | 310.034° NW | 2025-12-25 18:43:25.939Z | 276.998° WNW | 17.615° | 2025-12-25 18:47:25.939Z | 235.915° WSW |
| 5 mins | 2025-12-26 04:37:25.939Z | 104.828° ESE | 2025-12-26 04:39:25.939Z | 82.059° E | 16.091° | 2025-12-26 04:42:25.939Z | 49.992° ENE |
| 10 mins | 2025-12-26 06:19:25.939Z | 201.391° SSW | 2025-12-26 06:23:25.939Z | 269.057° W | 42.288° | 2025-12-26 06:29:25.939Z | 1.51° NNE |
| 4 mins | 2025-12-26 15:29:25.939Z | 46.506° ENE | 2025-12-26 15:31:25.939Z | 67.342° ENE | 13.642° | 2025-12-26 15:33:25.939Z | 87.851° E |
| 10 mins | 2025-12-26 17:12:25.939Z | 350.513° N | 2025-12-26 17:17:25.939Z | 199.69° SSW | 44.199° | 2025-12-26 17:22:25.939Z | 177.176° S |
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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