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: 10 hours ago
TLE from 10 hours ago
0 ITAMSAT
1 22826U 93061D 25261.11659680 .00000107 00000-0 57599-4 0 9998
2 22826 98.7218 323.0192 0009395 156.1109 204.0511 14.31245819668399Epoch: 2025-09-18T02:47Z
TLE epoch observation values (Epoch: 2025-09-18T02:47:53.963Z)
Latitude
-0.00006°
Longitude
-76.23844°
Altitude
796.649 km
Speed
7.452 km/s
True Right ascension
21h 32m 04s
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
06:03:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.443 km
Perigee altitude
777.984 km
Semi-major axis
7,162.851 km
Eccentricity
0.00094
Inclination
98.7218°
RAAN
323.0192°
Arg. of periapsis
156.1109°
True anomaly
204.00727°
Mean anomaly
204.0511°
Eccentric anomaly
204.02918°
Mean motion
3.58026 °/min
Orbital period
100.55 mins
BSTAR
0.000057599
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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 | 2025-09-18 16:48:09.981Z | 24.015° NE | 2025-09-18 16:52:09.981Z | 85.191° E | 39.898° | 2025-09-18 16:57:09.981Z | 179.375° S |
| 5 mins | 2025-09-18 18:29:09.981Z | 327.271° NNW | 2025-09-18 18:31:09.981Z | 300.877° NW | 16.742° | 2025-09-18 18:34:09.981Z | 262.022° W |
| 9 mins | 2025-09-19 04:05:09.981Z | 160.922° S | 2025-09-19 04:09:09.981Z | 103.267° ESE | 44.632° | 2025-09-19 04:14:09.981Z | 348.564° 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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