ITAMSAT, 22826
Orbit data source: Space-Track
ITAMSAT, 22826 is a payload satellite owned by Satellife (IT) in SSO that was launched on Sun, 26 Sep 1993 UTC via an ARIANE 40 launch vehicle from the French Guiana (FRGUI). 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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22826 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ITRelated business
Manufacturer
SSTL
Mission
Partially operational Commercial Communications
Bus & Motor
UOSAT, Unknown motor
Mass
50 kg wet, 50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Ant, 3.3 m
Radar Cross Section
0.597 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 ITAMSAT
1 22826U 93061D 26040.12491639 .00000147 00000-0 72232-4 0 9998
2 22826 98.6994 107.4093 0009988 99.2489 260.9824 14.31326415688997Epoch: 2026-02-09T02:59Z
TLE epoch observation values (Epoch: 2026-02-09T02:59:52.776Z)
Latitude
0.00002°
Longitude
-76.78483°
Altitude
791.36 km
Speed
7.457 km/s
True Right ascension
07h 09m 38s
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
17:54:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.598 km
Perigee altitude
777.29 km
Semi-major axis
7,162.581 km
Eccentricity
0.001
Inclination
98.6994°
RAAN
107.4093°
Arg. of periapsis
99.2489°
True anomaly
260.86938°
Mean anomaly
260.9824°
Eccentric anomaly
260.92589°
Mean motion
3.58046 °/min
Orbital period
100.55 mins
BSTAR
0.000072232
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Other satellites on launch #61 in the year 1993 (1993-09-26 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.ITAMSAT 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-02-09 16:59:38.183Z | 21.806° NNE | 2026-02-09 17:04:38.183Z | 119.141° SE | 40.749° | 2026-02-09 17:08:38.183Z | 179.865° S |
| 4 mins | 2026-02-09 18:41:38.183Z | 319.493° NNW | 2026-02-09 18:43:38.183Z | 291.981° WNW | 16.011° | 2026-02-09 18:45:38.183Z | 266.699° W |
| 8 mins | 2026-02-10 04:17:38.183Z | 162.386° S | 2026-02-10 04:21:38.183Z | 1.71° NNE | 43.791° | 2026-02-10 04:25:38.183Z | 347.811° 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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