OBJECT AE, 64556
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 AE, 64556 is a satellite in SSO that was launched on Mon, 23 Jun 2025 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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64556 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OBJECT AE
1 64556U 25135AE 25328.30425481 .00010301 00000-0 46175-3 0 9990
2 64556 97.4612 80.8977 0003011 75.8916 284.2654 15.21413062 23749Epoch: 2025-11-24T07:18Z
TLE epoch observation values (Epoch: 2025-11-24T07:18:07.615Z)
Latitude
-0.00005°
Longitude
-92.14017°
Altitude
504.158 km
Speed
7.612 km/s
True Right ascension
05h 23m 35s
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
14:20:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.614 km
Perigee altitude
496.473 km
Semi-major axis
6,876.681 km
Eccentricity
0.0003
Inclination
97.4612°
RAAN
80.8977°
Arg. of periapsis
75.8916°
True anomaly
284.23196°
Mean anomaly
284.2654°
Eccentric anomaly
284.24868°
Mean motion
3.80605 °/min
Orbital period
94.59 mins
BSTAR
0.00046175
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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 AE 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 | 2025-11-24 20:29:15.263Z | 13.814° NNE | 2025-11-24 20:32:15.263Z | 37.836° NE | 43.957° | 2025-11-24 20:35:15.263Z | 189.865° SSW |
| 4 mins | 2025-11-25 07:08:15.263Z | 113.867° SE | 2025-11-25 07:10:15.263Z | 56.907° ENE | 25.862° | 2025-11-25 07:12:15.263Z | 16.698° NNE |
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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