DECAYED
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TAUSAT-2, 55073 (Decayed)

Orbit data source: Space-Track

TAUSAT-2, 55073 was a payload satellite owned by Tel Aviv U. (IL) in LEO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

Not visible in the next 10 days
Identifier
55073, 2023-001BS
Orbit
Decayed
Country
Flag of UnknownUnknown / ISRA
Related business
Flag of ILTel Aviv University (IL)
Manufacturer
Tel Aviv U.
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2023-01-03 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 8 months ago

TLE from 8 months ago
0 TAUSAT-2
1 55073U 23001BS  25081.69089697  .10081506  24974-5  10714-2 0  9993
2 55073  97.3435 159.2003 0011744 269.6525  90.3427 16.37417385124057
Epoch: 2025-03-22T16:34Z
TLE epoch observation values (Epoch: 2025-03-22T16:34:53.498Z)
Latitude
-0.00005°
Longitude
90.04506°
Altitude
175.986 km
Speed
7.801 km/s
True Right ascension
10h 36m 48s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
05:38:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
177.18 km
Perigee altitude
161.801 km
Semi-major axis
6,547.627 km
Eccentricity
0.00117
Inclination
97.3435°
RAAN
159.2003°
Arg. of periapsis
269.6525°
True anomaly
90.47727°
Mean anomaly
90.3427°
Eccentric anomaly
90.40999°
Mean motion
4.09654 °/min
Orbital period
87.88 mins
BSTAR
0.0010714
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