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: 12 hours ago
TLE from 12 hours ago
0 ITAMSAT
1 22826U 93061D 25258.11050615 .00000075 00000-0 45244-4 0 9995
2 22826 98.7223 320.0016 0009226 164.5493 195.5973 14.31244804667960Epoch: 2025-09-15T02:39Z
TLE epoch observation values (Epoch: 2025-09-15T02:39:07.731Z)
Latitude
-0.00001°
Longitude
-74.10047°
Altitude
796.872 km
Speed
7.452 km/s
True Right ascension
21h 20m 00s
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
06:52:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.326 km
Perigee altitude
778.109 km
Semi-major axis
7,162.854 km
Eccentricity
0.00092
Inclination
98.7223°
RAAN
320.0016°
Arg. of periapsis
164.5493°
True anomaly
195.56891°
Mean anomaly
195.5973°
Eccentric anomaly
195.5831°
Mean motion
3.58026 °/min
Orbital period
100.55 mins
BSTAR
0.000045244
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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 | 2025-09-15 16:39:27.641Z | 27.916° NE | 2025-09-15 16:43:27.641Z | 87.425° E | 36.152° | 2025-09-15 16:48:27.641Z | 173.024° S |
| 6 mins | 2025-09-15 18:20:27.641Z | 330.163° NNW | 2025-09-15 18:22:27.641Z | 302.18° NW | 19.37° | 2025-09-15 18:26:27.641Z | 249.933° W |
| 8 mins | 2025-09-16 03:57:27.641Z | 151.148° SSE | 2025-09-16 04:00:27.641Z | 89.461° E | 42.775° | 2025-09-16 04:05:27.641Z | 352.228° 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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