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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Terran Orbital
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
0.4 kg wet, 0.2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.6 m
Radar Cross Section
0.100 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 25338.18174390 .00018664 00000-0 15801-2 0 9991
2 62713 97.7252 56.3983 0003691 76.3792 283.7841 14.98052068 48334Epoch: 2025-12-04T04:21Z
TLE epoch observation values (Epoch: 2025-12-04T04:21:42.672Z)
Latitude
-0.00007°
Longitude
-82.27136°
Altitude
575.356 km
Speed
7.573 km/s
True Right ascension
03h 45m 35s
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
13:00:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.489 km
Perigee altitude
567.36 km
Semi-major axis
6,948.061 km
Eccentricity
0.00037
Inclination
97.7252°
RAAN
56.3983°
Arg. of periapsis
76.3792°
True anomaly
283.74302°
Mean anomaly
283.7841°
Eccentric anomaly
283.76356°
Mean motion
3.74755 °/min
Orbital period
96.06 mins
BSTAR
0.0015801
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-05 17:47:38.966Z | 27.786° NE | 2025-12-05 17:51:38.966Z | 107.338° ESE | 32.771° | 2025-12-05 17:54:38.966Z | 165.912° S |
| 5 mins | 2025-12-06 04:36:38.966Z | 109.199° ESE | 2025-12-06 04:38:38.966Z | 68.983° E | 22.14° | 2025-12-06 04:41:38.966Z | 17.427° NNE |
| 5 mins | 2025-12-06 06:11:38.966Z | 222.607° SW | 2025-12-06 06:13:38.966Z | 262.786° W | 22.48° | 2025-12-06 06:16:38.966Z | 316.481° 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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