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, 0.2 m
Radar Cross Section
0.140 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 TEMISAT
1 22783U 93055B 26132.26839161 .00000055 00000-0 36453-4 0 9999
2 22783 82.5501 326.4628 0021811 311.8774 48.0524 13.83893765650748Epoch: 2026-05-12T06:26Z
TLE epoch observation values (Epoch: 2026-05-12T06:26:29.035Z)
Latitude
-0.00005°
Longitude
-0.20339°
Altitude
942.343 km
Speed
7.386 km/s
True Right ascension
21h 45m 51s
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
23:51:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
963.238 km
Perigee altitude
931.283 km
Semi-major axis
7,325.397 km
Eccentricity
0.00218
Inclination
82.5501°
RAAN
326.4628°
Arg. of periapsis
311.8774°
True anomaly
48.23863°
Mean anomaly
48.0524°
Eccentric anomaly
48.14548°
Mean motion
3.46176 °/min
Orbital period
103.99 mins
BSTAR
0.000036453
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-05-13 00:21:48.286Z | 1.61° NNE | 2026-05-13 00:27:48.286Z | 79.074° E | 39.091° | 2026-05-13 00:32:48.286Z | 153.016° SSE |
| 7 mins | 2026-05-13 02:08:48.286Z | 314.371° NW | 2026-05-13 02:11:48.286Z | 280.87° WNW | 19.814° | 2026-05-13 02:15:48.286Z | 235.235° WSW |
| 4 mins | 2026-05-13 12:06:48.286Z | 95.468° ESE | 2026-05-13 12:07:48.286Z | 84.666° E | 14.086° | 2026-05-13 12:10:48.286Z | 53.673° ENE |
| 10 mins | 2026-05-13 13:47:48.286Z | 194.778° SSW | 2026-05-13 13:51:48.286Z | 243.377° WSW | 43.598° | 2026-05-13 13:57:48.286Z | 3.671° NNE |
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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