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: 5 hours ago
TLE from 5 hours ago
0 OBJECT A
1 60203U 24125A 25298.49413203 .00034933 00000-0 77591-3 0 9991
2 60203 97.2578 149.2870 0016736 3.2076 356.9276 15.43466677 73189Epoch: 2025-10-25T11:51Z
TLE epoch observation values (Epoch: 2025-10-25T11:51:33.007Z)
Latitude
-0.00006°
Longitude
-62.7244°
Altitude
427.623 km
Speed
7.661 km/s
True Right ascension
09h 57m 08s
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
11:41:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
444.214 km
Perigee altitude
421.417 km
Semi-major axis
6,810.952 km
Eccentricity
0.00167
Inclination
97.2578°
RAAN
149.287°
Arg. of periapsis
3.2076°
True anomaly
356.9173°
Mean anomaly
356.9276°
Eccentric anomaly
356.92245°
Mean motion
3.86128 °/min
Orbital period
93.23 mins
BSTAR
0.00077591
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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 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 | 2025-10-26 02:26:24.914Z | 51.504° ENE | 2025-10-26 02:28:24.914Z | 102.537° ESE | 22.731° | 2025-10-26 02:30:24.914Z | 147.017° SSE |
| 4 mins | 2025-10-26 14:27:24.914Z | 191.604° SSW | 2025-10-26 14:28:24.914Z | 222.806° SW | 37.838° | 2025-10-26 14:31:24.914Z | 337.264° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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