OBJECT AG, 59128
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 AG, 59128 is a satellite in SSO that was launched on Mon, 04 Mar 2024 UTC via an FALCON 9 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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59128 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.080 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 OBJECT AG
1 59128U 24043AG 25293.85124087 .00011094 00000-0 40699-3 0 9990
2 59128 97.5345 63.6717 0010834 13.6577 346.4953 15.28087555 90510Epoch: 2025-10-20T20:25Z
TLE epoch observation values (Epoch: 2025-10-20T20:25:47.211Z)
Latitude
-0.00002°
Longitude
87.67737°
Altitude
477.4 km
Speed
7.631 km/s
True Right ascension
04h 14m 41s
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
04:08:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.919 km
Perigee altitude
471.062 km
Semi-major axis
6,856.627 km
Eccentricity
0.00108
Inclination
97.5345°
RAAN
63.6717°
Arg. of periapsis
13.6577°
True anomaly
346.46627°
Mean anomaly
346.4953°
Eccentric anomaly
346.48079°
Mean motion
3.82276 °/min
Orbital period
94.17 mins
BSTAR
0.00040699
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Other satellites on launch #43 in the year 2024 (2024-03-04 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 AG 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-21 09:08:40.398Z | 197.108° SSW | 2025-10-21 09:10:40.398Z | 272.286° WNW | 36.019° | 2025-10-21 09:13:40.398Z | 334.937° NNW |
| 5 mins | 2025-10-21 22:08:40.398Z | 342.476° N | 2025-10-21 22:10:40.398Z | 286.722° WNW | 30.349° | 2025-10-21 22:13:40.398Z | 221.795° SW |
| 4 mins | 2025-10-22 08:43:40.398Z | 153.787° SSE | 2025-10-22 08:44:40.398Z | 132.213° SE | 41.015° | 2025-10-22 08:47:40.398Z | 353.977° 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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