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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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: 23 hours ago
TLE from 23 hours ago
0 ITAMSAT
1 22826U 93061D 26309.67110798 .00000067 00000-0 42041-4 0 9996
2 22826 98.6677 16.8486 0009405 34.7238 325.4557 14.31401477727552Epoch: 2026-11-05T16:06Z
TLE epoch observation values (Epoch: 2026-11-05T16:06:23.729Z)
Latitude
-0.00004°
Longitude
90.34801°
Altitude
784.432 km
Speed
7.464 km/s
True Right ascension
01h 07m 23s
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
11:21:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
790.928 km
Perigee altitude
777.455 km
Semi-major axis
7,162.328 km
Eccentricity
0.00094
Inclination
98.6677°
RAAN
16.8486°
Arg. of periapsis
34.7238°
True anomaly
325.39453°
Mean anomaly
325.4557°
Eccentric anomaly
325.42512°
Mean motion
3.58065 °/min
Orbital period
100.54 mins
BSTAR
0.000042041
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-06 16:12:18.926Z | 57.296° ENE | 2026-11-06 16:15:18.926Z | 93.246° ESE | 15.125° | 2026-11-06 16:17:18.926Z | 118.076° SE |
| 8 mins | 2026-11-06 17:51:18.926Z | 2.778° NNE | 2026-11-06 17:55:18.926Z | 266.283° W | 60.647° | 2026-11-06 17:59:18.926Z | 209.196° SW |
| 6 mins | 2026-11-07 03:30:18.926Z | 99.79° ESE | 2026-11-07 03:32:18.926Z | 70.552° E | 22.223° | 2026-11-07 03:36:18.926Z | 17.053° NNE |
| 8 mins | 2026-11-07 05:08:18.926Z | 196.402° SSW | 2026-11-07 05:11:18.926Z | 246.382° WSW | 42.925° | 2026-11-07 05:16:18.926Z | 331.561° 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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