DECAYED
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NORSAT-TD, 56194 (Decayed)

Orbit data source: Space-Track

NORSAT-TD, 56194 was a payload satellite owned by NSC (NO) in LEO that was launched on Sat, 15 Apr 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
56194, 2023-054S
Orbit
Decayed
Country
Flag of NONO / NOR
Related business
Manufacturer
UTIAS-SFL
Mission
Decayed Civil Com/Tech
Bus & Motor
DEFIANT, Unknown motor
Mass
35 kg wet, 35 kg dry
Launch date (UTC)
2023-04-15 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.4 m
Radar Cross Section
0.165 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 months ago

TLE from 9 months ago
0 NORSAT-TD
1 56194U 23054S   25137.69058252  .07253072  25308-5  57328-3 0  9991
2 56194  97.3058  49.8020 0009374 227.7343 132.3162 16.40099231118095
Epoch: 2025-05-17T16:34Z
TLE epoch observation values (Epoch: 2025-05-17T16:34:26.329Z)
Latitude
-0.0001°
Longitude
-74.43597°
Altitude
172.927 km
Speed
7.8 km/s
True Right ascension
03h 19m 12s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
22:38:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
168.473 km
Perigee altitude
156.211 km
Semi-major axis
6,540.479 km
Eccentricity
0.00094
Inclination
97.3058°
RAAN
49.802°
Arg. of periapsis
227.7343°
True anomaly
132.39557°
Mean anomaly
132.3162°
Eccentric anomaly
132.35589°
Mean motion
4.10326 °/min
Orbital period
87.74 mins
BSTAR
0.00057328
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Computing Atmospheric mass density...

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