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: 11 hours ago
TLE from 11 hours ago
0 SATGUS
1 62713U 25009DJ 26238.16556698 .00006126 00000-0 47155-3 0 9992
2 62713 97.6928 318.8755 0003259 222.9525 137.1445 15.02026413 88066Epoch: 2026-08-26T03:58Z
TLE epoch observation values (Epoch: 2026-08-26T03:58:24.987Z)
Latitude
-0.00004°
Longitude
-75.15108°
Altitude
565.365 km
Speed
7.578 km/s
True Right ascension
21h 15m 30s
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
06:22:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
559.911 km
Perigee altitude
555.39 km
Semi-major axis
6,935.788 km
Eccentricity
0.00033
Inclination
97.6928°
RAAN
318.8755°
Arg. of periapsis
222.9525°
True anomaly
137.16989°
Mean anomaly
137.1445°
Eccentric anomaly
137.1572°
Mean motion
3.7575 °/min
Orbital period
95.81 mins
BSTAR
0.00047155
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-26 17:21:04.726Z | 54.452° ENE | 2026-08-26 17:23:04.726Z | 85.536° E | 15.872° | 2026-08-26 17:25:04.726Z | 121.04° SE |
| 6 mins | 2026-08-26 18:56:04.726Z | 343.576° N | 2026-08-26 18:58:04.726Z | 302.773° NW | 28.408° | 2026-08-26 19:02:04.726Z | 223.799° SW |
| 6 mins | 2026-08-27 05:41:04.726Z | 179.885° S | 2026-08-27 05:44:04.726Z | 276.152° WNW | 41.875° | 2026-08-27 05:47:04.726Z | 339.344° N |
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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