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.
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56194 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
UTIAS-SFL
Mission
Decayed Civil Com/Tech
Bus & Motor
DEFIANT, Unknown motor
Mass
35 kg wet, 35 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.4 m
Radar Cross Section
0.165 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 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 16.40099231118095Epoch: 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
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
02:20:16
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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Other satellites on launch #54 in the year 2023 (2023-04-15 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.NORSAT-TD Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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