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: 22 hours ago
TLE from 22 hours ago
0 ITAMSAT
1 22826U 93061D 25314.59636089 .00000253 00000-0 11275-3 0 9999
2 22826 98.7138 16.6770 0009021 12.8801 347.2610 14.31277439676044Epoch: 2025-11-10T14:18Z
TLE epoch observation values (Epoch: 2025-11-10T14:18:45.580Z)
Latitude
-0.0001°
Longitude
111.9921°
Altitude
784.088 km
Speed
7.465 km/s
True Right ascension
01h 06m 42s
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
09:01:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.069 km
Perigee altitude
778.146 km
Semi-major axis
7,162.745 km
Eccentricity
0.0009
Inclination
98.7138°
RAAN
16.677°
Arg. of periapsis
12.8801°
True anomaly
347.23818°
Mean anomaly
347.261°
Eccentric anomaly
347.24959°
Mean motion
3.58034 °/min
Orbital period
100.55 mins
BSTAR
0.00011275
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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 | 2025-11-11 16:04:47.109Z | 48.46° ENE | 2025-11-11 16:08:47.109Z | 101.495° ESE | 19.149° | 2025-11-11 16:11:47.109Z | 138.694° SSE |
| 8 mins | 2025-11-11 17:44:47.109Z | 351.933° N | 2025-11-11 17:47:47.109Z | 293.27° NW | 35.747° | 2025-11-11 17:52:47.109Z | 217.665° SW |
| 7 mins | 2025-11-12 03:22:47.109Z | 113.711° SE | 2025-11-12 03:25:47.109Z | 62.784° ENE | 26.189° | 2025-11-12 03:29:47.109Z | 9.341° NNE |
| 7 mins | 2025-11-12 05:01:47.109Z | 210.688° SW | 2025-11-12 05:04:47.109Z | 260.576° W | 27.922° | 2025-11-12 05:08:47.109Z | 321.774° 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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