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: 9 hours ago
TLE from 9 hours ago
0 ITAMSAT
1 22826U 93061D 25345.14568208 .00000237 00000-0 10637-3 0 9994
2 22826 98.7096 47.3082 0007823 276.4432 83.5860 14.31296550680418Epoch: 2025-12-11T03:29Z
TLE epoch observation values (Epoch: 2025-12-11T03:29:46.931Z)
Latitude
-0.00002°
Longitude
-85.2432°
Altitude
789.708 km
Speed
7.459 km/s
True Right ascension
03h 09m 13s
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
10:37:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
790.147 km
Perigee altitude
778.94 km
Semi-major axis
7,162.681 km
Eccentricity
0.00078
Inclination
98.7096°
RAAN
47.3082°
Arg. of periapsis
276.4432°
True anomaly
83.67509°
Mean anomaly
83.586°
Eccentric anomaly
83.63055°
Mean motion
3.58039 °/min
Orbital period
100.55 mins
BSTAR
0.00010637
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-11 15:51:50.879Z | 64.016° ENE | 2025-12-11 15:53:50.879Z | 88.064° E | 13.843° | 2025-12-11 15:55:50.879Z | 113.048° SE |
| 9 mins | 2025-12-11 17:29:50.879Z | 5.345° NNE | 2025-12-11 17:33:50.879Z | 291.295° WNW | 42.294° | 2025-12-11 17:38:50.879Z | 206.241° SW |
| 6 mins | 2025-12-12 03:08:50.879Z | 103.568° ESE | 2025-12-12 03:11:50.879Z | 60.892° ENE | 20.32° | 2025-12-12 03:14:50.879Z | 21.214° NNE |
| 8 mins | 2025-12-12 04:46:50.879Z | 192.202° SSW | 2025-12-12 04:50:50.879Z | 265.357° W | 35.682° | 2025-12-12 04:54:50.879Z | 330.262° 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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