NAVSTAR 84 (USA 545), 64202
Orbit data source: Space-Track
NAVSTAR 84 (USA 545), 64202 is a payload satellite owned by USSF SSC (US) in MEO that was launched on Fri, 30 May 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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64202 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
LMSS Denver
Mission
Operational Defense Navigation
Bus & Motor
A2100, LEROS-1C?
Mass
4,352 kg wet, ~2,160 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 7.0 m
Radar Cross Section
13.646 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 NAVSTAR 84 (USA 545)
1 64202U 25116A 26155.12197520 -.00000073 00000-0 00000+0 0 9995
2 64202 55.2255 31.6566 0008467 337.9312 19.6121 2.00577105 7600Epoch: 2026-06-04T02:55Z
TLE epoch observation values (Epoch: 2026-06-04T02:55:38.657Z)
Latitude
-2.03908°
Longitude
93.77882°
Altitude
20,160.45 km
Speed
3.877 km/s
True Right ascension
02h 01m 02s
True Declination
-2° 02' 09"
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
18:11:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,203.503 km
Perigee altitude
20,158.528 km
Semi-major axis
26,559.152 km
Eccentricity
0.00085
Inclination
55.2255°
RAAN
31.6566°
Arg. of periapsis
337.9312°
True anomaly
19.6447°
Mean anomaly
19.6121°
Eccentric anomaly
19.6284°
Mean motion
0.50144 °/min
Orbital period
717.93 mins
BSTAR
0
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Other satellites on launch #116 in the year 2025 (2025-05-30 UTC)
No other RSOs were in this launch
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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.NAVSTAR 84 (USA 545) Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 301 mins | 2026-06-04 13:57:57.093Z | 164.322° S | 2026-06-04 16:25:57.093Z | 95.849° ESE | 41.559° | 2026-06-04 18:58:57.093Z | 50.499° ENE |
| 119 mins | 2026-06-05 06:14:57.093Z | 321.415° NNW | 2026-06-05 07:11:57.093Z | 298.997° NW | 16.476° | 2026-06-05 08:13:57.093Z | 272.577° WNW |
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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