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: 13 hours ago
TLE from 13 hours ago
0 TEMISAT
1 22783U 93055B 26184.97552800 .00000067 00000-0 47135-4 0 9998
2 22783 82.5520 284.6307 0023364 158.6071 201.6071 13.83896985658031Epoch: 2026-07-03T23:24Z
TLE epoch observation values (Epoch: 2026-07-03T23:24:45.619Z)
Latitude
-0.00002°
Longitude
11.44476°
Altitude
968.926 km
Speed
7.359 km/s
True Right ascension
18h 58m 31s
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
00:38:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
964.364 km
Perigee altitude
930.134 km
Semi-major axis
7,325.386 km
Eccentricity
0.00234
Inclination
82.552°
RAAN
284.6307°
Arg. of periapsis
158.6071°
True anomaly
201.50878°
Mean anomaly
201.6071°
Eccentric anomaly
201.55791°
Mean motion
3.46176 °/min
Orbital period
103.99 mins
BSTAR
0.000047135
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-07-04 17:21:00.833Z | 22.609° NE | 2026-07-04 17:25:00.833Z | 66.596° ENE | 20.762° | 2026-07-04 17:29:00.833Z | 114.438° SE |
| 10 mins | 2026-07-04 19:06:00.833Z | 337.473° NNW | 2026-07-04 19:10:00.833Z | 283.673° WNW | 37.242° | 2026-07-04 19:16:00.833Z | 195.238° SSW |
| 10 mins | 2026-07-05 06:46:00.833Z | 155.577° SSE | 2026-07-05 06:50:00.833Z | 99.593° ESE | 35.348° | 2026-07-05 06:56:00.833Z | 20.499° NNE |
| 8 mins | 2026-07-05 08:32:00.833Z | 245.066° WSW | 2026-07-05 08:35:00.833Z | 282.19° WNW | 23.198° | 2026-07-05 08:40:00.833Z | 340.658° N |
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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