SATGUS, 62713
Orbit data source: Space-Track
SATGUS, 62713 is an American payload satellite in SSO that was launched on Tue, 14 Jan 2025 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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62713 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Terran Orbital
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.8 m
Radar Cross Section
0.123 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SATGUS
1 62713U 25009DJ 26287.18875673 .00006638 00000-0 50419-3 0 9990
2 62713 97.6826 7.4752 0003489 80.4090 279.7529 15.02504626 95421Epoch: 2026-10-14T04:31Z
TLE epoch observation values (Epoch: 2026-10-14T04:31:48.581Z)
Latitude
-0.00002°
Longitude
-83.21927°
Altitude
561.825 km
Speed
7.581 km/s
True Right ascension
00h 29m 54s
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
03:25:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
558.597 km
Perigee altitude
553.758 km
Semi-major axis
6,934.314 km
Eccentricity
0.00035
Inclination
97.6826°
RAAN
7.4752°
Arg. of periapsis
80.409°
True anomaly
279.71349°
Mean anomaly
279.7529°
Eccentric anomaly
279.7332°
Mean motion
3.7587 °/min
Orbital period
95.78 mins
BSTAR
0.00050419
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.SATGUS 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-15 17:52:05.471Z | 35.448° NE | 2026-10-15 17:55:05.471Z | 103.572° ESE | 37.014° | 2026-10-15 17:58:05.471Z | 163.06° S |
| 4 mins | 2026-10-16 04:39:05.471Z | 92.893° ESE | 2026-10-16 04:40:05.471Z | 72.479° E | 20.921° | 2026-10-16 04:43:05.471Z | 21.139° NNE |
| 5 mins | 2026-10-16 06:13:05.471Z | 220.497° SW | 2026-10-16 06:15:05.471Z | 265.812° W | 27.533° | 2026-10-16 06:18:05.471Z | 320.403° NNW |
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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