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: 17 hours ago
TLE from 17 hours ago
0 ITAMSAT
1 22826U 93061D 26305.61682528 .00000046 00000-0 34267-4 0 9999
2 22826 98.6680 12.8031 0009604 45.6748 314.5221 14.31400594726977Epoch: 2026-11-01T14:48Z
TLE epoch observation values (Epoch: 2026-11-01T14:48:13.704Z)
Latitude
0.00003°
Longitude
109.84036°
Altitude
785.162 km
Speed
7.464 km/s
True Right ascension
00h 51m 12s
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
03:23:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.073 km
Perigee altitude
777.316 km
Semi-major axis
7,162.331 km
Eccentricity
0.00096
Inclination
98.668°
RAAN
12.8031°
Arg. of periapsis
45.6748°
True anomaly
314.44357°
Mean anomaly
314.5221°
Eccentric anomaly
314.48284°
Mean motion
3.58065 °/min
Orbital period
100.54 mins
BSTAR
0.000034267
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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 | 2026-11-02 16:34:04.905Z | 45.852° ENE | 2026-11-02 16:38:04.905Z | 103.869° ESE | 24.38° | 2026-11-02 16:41:04.905Z | 143.856° SSE |
| 7 mins | 2026-11-02 18:14:04.905Z | 346.344° N | 2026-11-02 18:17:04.905Z | 290.344° WNW | 38.471° | 2026-11-02 18:21:04.905Z | 227.65° WSW |
| 8 mins | 2026-11-03 03:51:04.905Z | 126.396° SE | 2026-11-03 03:55:04.905Z | 58.284° ENE | 34.308° | 2026-11-03 03:59:04.905Z | 5.726° NNE |
| 7 mins | 2026-11-03 05:31:04.905Z | 217.525° SW | 2026-11-03 05:34:04.905Z | 264.204° W | 26.998° | 2026-11-03 05:38:04.905Z | 319.542° 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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