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 25359.75611750 .00000145 00000-0 71683-4 0 9994
2 22826 98.7076 61.9538 0008117 228.1157 131.9334 14.31302685682502Epoch: 2025-12-25T18:08Z
TLE epoch observation values (Epoch: 2025-12-25T18:08:48.551Z)
Latitude
-0.00004°
Longitude
55.24492°
Altitude
794.2 km
Speed
7.454 km/s
True Right ascension
04h 07m 48s
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
22:22:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
790.337 km
Perigee altitude
778.709 km
Semi-major axis
7,162.66 km
Eccentricity
0.00081
Inclination
98.7076°
RAAN
61.9538°
Arg. of periapsis
228.1157°
True anomaly
132.00255°
Mean anomaly
131.9334°
Eccentric anomaly
131.96798°
Mean motion
3.5804 °/min
Orbital period
100.55 mins
BSTAR
0.000071683
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-26 04:20:45.257Z | 168.456° S | 2025-12-26 04:23:45.257Z | 194.373° SSW | 44.451° | 2025-12-26 04:28:45.257Z | 345.029° N |
| 7 mins | 2025-12-26 16:33:45.257Z | 42.213° NE | 2025-12-26 16:36:45.257Z | 93.412° ESE | 29.922° | 2025-12-26 16:40:45.257Z | 158.285° S |
| 6 mins | 2025-12-26 18:13:45.257Z | 333.723° NNW | 2025-12-26 18:15:45.257Z | 301.715° NW | 24.464° | 2025-12-26 18:19:45.257Z | 241.972° WSW |
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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