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: 2 days ago
TLE from 2 days ago
0 TEMISAT
1 22783U 93055B 25306.46613219 .00000073 00000-0 52413-4 0 9991
2 22783 82.5476 117.8704 0023880 123.2386 237.1067 13.83876888624356Epoch: 2025-11-02T11:11Z
TLE epoch observation values (Epoch: 2025-11-02T11:11:13.821Z)
Latitude
-0.00005°
Longitude
-91.91865°
Altitude
962.605 km
Speed
7.366 km/s
True Right ascension
07h 51m 28s
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
00:03:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
964.813 km
Perigee altitude
929.827 km
Semi-major axis
7,325.457 km
Eccentricity
0.00239
Inclination
82.5476°
RAAN
117.8704°
Arg. of periapsis
123.2386°
True anomaly
236.8773°
Mean anomaly
237.1067°
Eccentric anomaly
236.99196°
Mean motion
3.46171 °/min
Orbital period
103.99 mins
BSTAR
0.000052413
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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 | 2025-11-04 11:52:48.523Z | 173.401° S | 2025-11-04 11:57:48.523Z | 104.51° ESE | 42.472° | 2025-11-04 12:03:48.523Z | 13.537° NNE |
| 6 mins | 2025-11-04 13:40:48.523Z | 262.542° W | 2025-11-04 13:43:48.523Z | 296.71° NW | 16.649° | 2025-11-04 13:46:48.523Z | 328.358° NNW |
| 10 mins | 2025-11-04 22:46:48.523Z | 8.25° NNE | 2025-11-04 22:50:48.523Z | 68.033° E | 37.762° | 2025-11-04 22:56:48.523Z | 153.805° SSE |
| 7 mins | 2025-11-05 00:32:48.523Z | 309.067° NW | 2025-11-05 00:35:48.523Z | 271.557° WNW | 19.987° | 2025-11-05 00:39:48.523Z | 228.968° WSW |
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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