OBJECT AG, 64558
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, 64558 is a satellite in SSO that was launched on Mon, 23 Jun 2025 UTC launched 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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64558 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Communications
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Unknown
Shape & HBR
Box + 4 Pan, 1.0 m
Radar Cross Section
0.326 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 OBJECT AG
1 64558U 25135AG 25269.82955073 .00018365 00000-0 89055-3 0 9990
2 64558 97.4563 22.8332 0006074 14.1015 346.0388 15.18546819 14761Epoch: 2025-09-26T19:54Z
TLE epoch observation values (Epoch: 2025-09-26T19:54:33.183Z)
Latitude
0.00004°
Longitude
78.32422°
Altitude
509.257 km
Speed
7.612 km/s
True Right ascension
01h 31m 19s
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
21:09:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.384 km
Perigee altitude
503.019 km
Semi-major axis
6,885.339 km
Eccentricity
0.00061
Inclination
97.4563°
RAAN
22.8332°
Arg. of periapsis
14.1015°
True anomaly
346.02199°
Mean anomaly
346.0388°
Eccentric anomaly
346.0304°
Mean motion
3.79888 °/min
Orbital period
94.76 mins
BSTAR
0.00089055
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Other satellites on launch #135 in the year 2025 (2025-06-23 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 | 2025-09-27 07:07:16.972Z | 129.01° SE | 2025-09-27 07:10:16.972Z | 55.313° ENE | 26.928° | 2025-09-27 07:12:16.972Z | 15.337° NNE |
| 6 mins | 2025-09-27 20:12:16.972Z | 29.211° NE | 2025-09-27 20:15:16.972Z | 127.268° SE | 35.756° | 2025-09-27 20:18:16.972Z | 175.516° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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