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 Microgravity
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Trunc Cone, 0.7 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OBJECT AE
1 64556U 25135AE 25268.28871844 .00015208 00000-0 71490-3 0 9997
2 64556 97.4565 21.5161 0000808 257.0831 103.0314 15.19682277 14625Epoch: 2025-09-25T06:55Z
TLE epoch observation values (Epoch: 2025-09-25T06:55:45.273Z)
Latitude
0.00003°
Longitude
-86.77453°
Altitude
510.014 km
Speed
7.609 km/s
True Right ascension
01h 26m 03s
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
15:09:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.325 km
Perigee altitude
503.212 km
Semi-major axis
6,881.906 km
Eccentricity
0.00008
Inclination
97.4565°
RAAN
21.5161°
Arg. of periapsis
257.0831°
True anomaly
103.04042°
Mean anomaly
103.0314°
Eccentric anomaly
103.03591°
Mean motion
3.80172 °/min
Orbital period
94.69 mins
BSTAR
0.0007149
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-27 08:03:20.952Z | 197.566° SSW | 2025-09-27 08:05:20.952Z | 257.479° W | 35.338° | 2025-09-27 08:08:20.952Z | 331.689° NNW |
| 4 mins | 2025-09-27 21:08:20.952Z | 328.364° NNW | 2025-09-27 21:09:20.952Z | 303.12° NW | 25.874° | 2025-09-27 21:12:20.952Z | 232.603° WSW |
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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