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
Cyl + 1 Pan, 0.8 m
Radar Cross Section
2.062 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 OBJECT AG
1 59128U 24043AG 26034.27271245 .00008855 00000-0 30582-3 0 9990
2 59128 97.5424 170.4982 0010240 1.7483 358.3791 15.30137557106627Epoch: 2026-02-03T06:32Z
TLE epoch observation values (Epoch: 2026-02-03T06:32:42.355Z)
Latitude
-0.00006°
Longitude
-61.13429°
Altitude
471.485 km
Speed
7.634 km/s
True Right ascension
11h 21m 59s
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
17:08:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.375 km
Perigee altitude
465.345 km
Semi-major axis
6,850.497 km
Eccentricity
0.00102
Inclination
97.5424°
RAAN
170.4982°
Arg. of periapsis
1.7483°
True anomaly
358.37578°
Mean anomaly
358.3791°
Eccentric anomaly
358.37744°
Mean motion
3.8279 °/min
Orbital period
94.05 mins
BSTAR
0.00030582
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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 | 2026-02-03 21:14:26.865Z | 41.581° NE | 2026-02-03 21:17:26.865Z | 109.795° ESE | 23.889° | 2026-02-03 21:19:26.865Z | 150.253° SSE |
| 5 mins | 2026-02-04 09:21:26.865Z | 192.551° SSW | 2026-02-04 09:23:26.865Z | 237.303° WSW | 33.693° | 2026-02-04 09:26:26.865Z | 329.759° NNW |
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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