USA 485, 62756
Orbit data source: Space-Track
USA 485, 62756 is a payload satellite owned by NRO (US) in LEO that was launched on Tue, 21 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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62756 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Defense Imaging
Bus & Motor
STARSHIELD, Unknown motor
Mass
800 kg wet, ~750 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 2.3 m
Radar Cross Section
41.120 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 USA 485
1 62756U 25014X 26171.26385498 .00198011 00000-0 11883-2 0 9993
2 62756 43.0006 92.1427 0001627 268.0815 91.9869 15.76412194 81250Epoch: 2026-06-20T06:19Z
TLE epoch observation values (Epoch: 2026-06-20T06:19:57.070Z)
Latitude
0.00003°
Longitude
88.67396°
Altitude
340.424 km
Speed
7.706 km/s
True Right ascension
06h 08m 34s
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
07:23:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
343.695 km
Perigee altitude
341.508 km
Semi-major axis
6,720.739 km
Eccentricity
0.00016
Inclination
43.0006°
RAAN
92.1427°
Arg. of periapsis
268.0815°
True anomaly
92.00553°
Mean anomaly
91.9869°
Eccentric anomaly
91.99622°
Mean motion
3.93929 °/min
Orbital period
91.39 mins
BSTAR
0.0011883
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Other satellites on launch #14 in the year 2025 (2025-01-21 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.USA 485 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 | 2026-06-21 02:31:44.849Z | 289.461° WNW | 2026-06-21 02:33:44.849Z | 90.189° ESE | 44.185° | 2026-06-21 02:35:44.849Z | 106.857° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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