LEO 3, 57392
Orbit data source: Space-Track
LEO 3, 57392 is a payload satellite owned by Telesat (Loral) (CA) in SSO that was launched on Tue, 18 Jul 2023 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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57392 intel report (Beta)
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Identifier
Orbit
Country
CARelated business
Manufacturer
UTIAS-SFL
Mission
Partially operational Commercial Communications
Bus & Motor
DEFIANT, Unknown motor
Mass
30 kg wet, 30 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.6 m
Radar Cross Section
0.280 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 LEO 3
1 57392U 23100G 26287.07222173 -.00000033 00000-0 14048-4 0 9999
2 57392 99.5797 50.3711 0018956 71.2247 289.0953 13.68420563161904Epoch: 2026-10-14T01:43Z
TLE epoch observation values (Epoch: 2026-10-14T01:43:59.957Z)
Latitude
0.00001°
Longitude
1.74409°
Altitude
1,003.506 km
Speed
7.352 km/s
True Right ascension
03h 21m 29s
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
13:52:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,016.508 km
Perigee altitude
988.527 km
Semi-major axis
7,380.654 km
Eccentricity
0.0019
Inclination
99.5797°
RAAN
50.3711°
Arg. of periapsis
71.2247°
True anomaly
288.88987°
Mean anomaly
289.0953°
Eccentric anomaly
288.9926°
Mean motion
3.42295 °/min
Orbital period
105.17 mins
BSTAR
0.000014048
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Other satellites on launch #100 in the year 2023 (2023-07-18 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.LEO 3 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-10-14 19:54:26.326Z | 52.103° ENE | 2026-10-14 19:58:26.326Z | 94.575° ESE | 18.833° | 2026-10-14 20:02:26.326Z | 135.208° SSE |
| 11 mins | 2026-10-14 21:37:26.326Z | 6.767° NNE | 2026-10-14 21:42:26.326Z | 290.682° WNW | 65.625° | 2026-10-14 21:48:26.326Z | 208.562° SW |
| 10 mins | 2026-10-15 07:41:26.326Z | 138.84° SSE | 2026-10-15 07:46:26.326Z | 61.94° ENE | 50.371° | 2026-10-15 07:51:26.326Z | 357.97° N |
| 8 mins | 2026-10-15 09:26:26.326Z | 220.218° SW | 2026-10-15 09:30:26.326Z | 268.634° W | 24.629° | 2026-10-15 09:34:26.326Z | 313.996° NW |
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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