POSAT 1, 22829
Orbit data source: Space-Track
POSAT 1, 22829 is a payload satellite owned by INETI (PT) 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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22829 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
PT / PORRelated business
Manufacturer
SSTL
Mission
Non-operational Amateur 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: 6 hours ago
TLE from 6 hours ago
0 POSAT 1
1 22829U 93061G 25359.71336507 .00000127 00000-0 64242-4 0 9990
2 22829 98.6906 61.8398 0009838 173.5073 186.6239 14.31857451683227Epoch: 2025-12-25T17:07Z
TLE epoch observation values (Epoch: 2025-12-25T17:07:14.742Z)
Latitude
-0.00003°
Longitude
70.56393°
Altitude
795.462 km
Speed
7.452 km/s
True Right ascension
04h 07m 21s
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
22:19:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
789.715 km
Perigee altitude
775.626 km
Semi-major axis
7,160.808 km
Eccentricity
0.00098
Inclination
98.6906°
RAAN
61.8398°
Arg. of periapsis
173.5073°
True anomaly
186.61091°
Mean anomaly
186.6239°
Eccentric anomaly
186.6174°
Mean motion
3.58179 °/min
Orbital period
100.51 mins
BSTAR
0.000064242
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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.POSAT 1 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 | 2025-12-26 03:19:49.426Z | 116.532° SE | 2025-12-26 03:22:49.426Z | 75.66° E | 24.076° | 2025-12-26 03:26:49.426Z | 15.754° NNE |
| 8 mins | 2025-12-26 04:58:49.426Z | 202.187° SSW | 2025-12-26 05:02:49.426Z | 270.745° WNW | 30.284° | 2025-12-26 05:06:49.426Z | 326.542° NNW |
| 8 mins | 2025-12-26 17:11:49.426Z | 17.017° NNE | 2025-12-26 17:14:49.426Z | 58.945° ENE | 44.527° | 2025-12-26 17:19:49.426Z | 191.715° SSW |
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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