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, 0.6 m
Radar Cross Section
0.123 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 SATGUS
1 62713U 25009DJ 26080.58116221 .00011760 00000-0 94803-3 0 9999
2 62713 97.7121 162.7348 0005450 62.8410 297.3369 15.00044136 64423Epoch: 2026-03-21T13:56Z
TLE epoch observation values (Epoch: 2026-03-21T13:56:52.414Z)
Latitude
-0.00001°
Longitude
134.41659°
Altitude
568.078 km
Speed
7.578 km/s
True Right ascension
10h 50m 56s
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
07:03:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
567.549 km
Perigee altitude
559.983 km
Semi-major axis
6,941.903 km
Eccentricity
0.00055
Inclination
97.7121°
RAAN
162.7348°
Arg. of periapsis
62.841°
True anomaly
297.2814°
Mean anomaly
297.3369°
Eccentric anomaly
297.30915°
Mean motion
3.75254 °/min
Orbital period
95.94 mins
BSTAR
0.00094803
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-22 04:30:43.177Z | 107.458° ESE | 2026-03-22 04:32:43.177Z | 73.141° E | 18.565° | 2026-03-22 04:35:43.177Z | 22.64° NE |
| 5 mins | 2026-03-22 06:05:43.177Z | 215.525° SW | 2026-03-22 06:07:43.177Z | 260.118° W | 26.253° | 2026-03-22 06:10:43.177Z | 319.981° NNW |
| 6 mins | 2026-03-22 17:44:43.177Z | 39.927° NE | 2026-03-22 17:47:43.177Z | 110.53° ESE | 28.753° | 2026-03-22 17:50:43.177Z | 161.912° S |
| 4 mins | 2026-03-22 19:20:43.177Z | 318.204° NNW | 2026-03-22 19:21:43.177Z | 300.605° NW | 16.606° | 2026-03-22 19:24:43.177Z | 251.625° W |
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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