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, 0.7 m
Radar Cross Section
0.280 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 LEO 3
1 57392U 23100G 26092.87835396 -.00000022 00000-0 26086-4 0 9991
2 57392 99.5511 217.9410 0018001 206.9849 153.0361 13.68418599135349Epoch: 2026-04-02T21:04Z
TLE epoch observation values (Epoch: 2026-04-02T21:04:49.782Z)
Latitude
-0.00005°
Longitude
70.51307°
Altitude
1,019.923 km
Speed
7.336 km/s
True Right ascension
14h 31m 45s
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
07:50:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,015.809 km
Perigee altitude
989.237 km
Semi-major axis
7,380.66 km
Eccentricity
0.0018
Inclination
99.5511°
RAAN
217.941°
Arg. of periapsis
206.9849°
True anomaly
153.12944°
Mean anomaly
153.0361°
Eccentric anomaly
153.08279°
Mean motion
3.42295 °/min
Orbital period
105.17 mins
BSTAR
0.000026086
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-04-03 07:43:20.828Z | 145.694° SSE | 2026-04-03 07:49:20.828Z | 51.628° ENE | 39.726° | 2026-04-03 07:54:20.828Z | 355.072° N |
| 8 mins | 2026-04-03 09:29:20.828Z | 225.345° WSW | 2026-04-03 09:33:20.828Z | 271.495° WNW | 20.574° | 2026-04-03 09:37:20.828Z | 313.371° NW |
| 10 mins | 2026-04-03 20:30:20.828Z | 35.575° NE | 2026-04-03 20:35:20.828Z | 109.115° ESE | 32.517° | 2026-04-03 20:40:20.828Z | 165.937° S |
| 9 mins | 2026-04-03 22:14:20.828Z | 348.717° N | 2026-04-03 22:18:20.828Z | 298.175° NW | 28.073° | 2026-04-03 22:23:20.828Z | 237.501° WSW |
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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