OBJECT AG, 59128
Orbit data source: Space-Track
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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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, 0.9 m
Radar Cross Section
2.062 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 OBJECT AG
1 59128U 24043AG 26286.66397471 .00007171 00000-0 22458-3 0 9995
2 59128 97.5820 68.1115 0009656 171.5238 188.6169 15.33375837145265Epoch: 2026-10-13T15:56Z
TLE epoch observation values (Epoch: 2026-10-13T15:56:07.414Z)
Latitude
-0.00003°
Longitude
166.85581°
Altitude
475.388 km
Speed
7.624 km/s
True Right ascension
04h 32m 26s
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
00:36:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.31 km
Perigee altitude
456.099 km
Semi-major axis
6,840.842 km
Eccentricity
0.00097
Inclination
97.582°
RAAN
68.1115°
Arg. of periapsis
171.5238°
True anomaly
188.60034°
Mean anomaly
188.6169°
Eccentric anomaly
188.60862°
Mean motion
3.836 °/min
Orbital period
93.85 mins
BSTAR
0.00022458
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-14 09:17:33.396Z | 147.529° SSE | 2026-10-14 09:20:33.396Z | 71.747° E | 48.493° | 2026-10-14 09:23:33.396Z | 0.929° NNE |
| 4 mins | 2026-10-14 22:16:33.396Z | 30.255° NE | 2026-10-14 22:18:33.396Z | 137.762° SSE | 54.498° | 2026-10-14 22:20:33.396Z | 178.215° S |
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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