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: 5 hours ago
TLE from 5 hours ago
0 ITAMSAT
1 22826U 93061D 25308.44450250 .00000174 00000-0 82778-4 0 9999
2 22826 98.7146 10.5071 0009361 30.2640 329.9081 14.31273532675163Epoch: 2025-11-04T10:40Z
TLE epoch observation values (Epoch: 2025-11-04T10:40:05.016Z)
Latitude
-0.00012°
Longitude
166.55479°
Altitude
784.604 km
Speed
7.465 km/s
True Right ascension
00h 42m 01s
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
11:57:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.326 km
Perigee altitude
777.916 km
Semi-major axis
7,162.758 km
Eccentricity
0.00094
Inclination
98.7146°
RAAN
10.5071°
Arg. of periapsis
30.264°
True anomaly
329.85426°
Mean anomaly
329.9081°
Eccentric anomaly
329.88119°
Mean motion
3.58033 °/min
Orbital period
100.55 mins
BSTAR
0.000082778
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-04 16:18:03.751Z | 44.46° NE | 2025-11-04 16:21:03.751Z | 86.329° E | 24.444° | 2025-11-04 16:25:03.751Z | 147.499° SSE |
| 7 mins | 2025-11-04 17:58:03.751Z | 343.26° N | 2025-11-04 18:01:03.751Z | 288.788° WNW | 29.616° | 2025-11-04 18:05:03.751Z | 230.602° WSW |
| 8 mins | 2025-11-05 03:35:03.751Z | 130.403° SE | 2025-11-05 03:39:03.751Z | 57.369° ENE | 31.745° | 2025-11-05 03:43:03.751Z | 3.638° NNE |
| 6 mins | 2025-11-05 05:16:03.751Z | 231.661° WSW | 2025-11-05 05:18:03.751Z | 263.771° W | 22.046° | 2025-11-05 05:22:03.751Z | 317.19° NNW |
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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