OBJECT A, 60203
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT A, 60203 is an American satellite in SSO that was launched on Thu, 04 Jul 2024 UTC via an FIREFLY ALPHA launch vehicle from the Air Force Western Test Range (AFWTR). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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60203 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
None
Manufacturer
Unknown
Mission
Operational Amateur Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.025 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 OBJECT A
1 60203U 24125A 26035.84252926 .00048533 00000-0 79081-3 0 9990
2 60203 97.2470 251.9158 0013129 348.0488 12.0452 15.52388279 89016Epoch: 2026-02-04T20:13Z
TLE epoch observation values (Epoch: 2026-02-04T20:13:14.528Z)
Latitude
0.00005°
Longitude
173.60195°
Altitude
404.177 km
Speed
7.673 km/s
True Right ascension
16h 47m 39s
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
14:25:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
415.579 km
Perigee altitude
397.763 km
Semi-major axis
6,784.808 km
Eccentricity
0.00131
Inclination
97.247°
RAAN
251.9158°
Arg. of periapsis
348.0488°
True anomaly
12.07665°
Mean anomaly
12.0452°
Eccentric anomaly
12.06092°
Mean motion
3.88362 °/min
Orbital period
92.7 mins
BSTAR
0.00079081
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Other satellites on launch #125 in the year 2024 (2024-07-04 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.OBJECT A Visibility
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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. |
|---|---|---|---|---|---|---|---|
| OBJECT A is likely not visible in the next few days. |
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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