OBJECT AJ, 64560
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 AJ, 64560 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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64560 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
Box, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OBJECT AJ
1 64560U 25135AJ 25268.79575970 .00011384 00000-0 11287-2 0 9997
2 64560 97.7556 21.5716 0001614 89.9055 270.2348 14.91949981 14435Epoch: 2025-09-25T19:05Z
TLE epoch observation values (Epoch: 2025-09-25T19:05:53.638Z)
Latitude
-0.00008°
Longitude
90.24636°
Altitude
594.893 km
Speed
7.562 km/s
True Right ascension
01h 26m 17s
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
17:09:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.999 km
Perigee altitude
587.75 km
Semi-major axis
6,967.011 km
Eccentricity
0.00016
Inclination
97.7556°
RAAN
21.5716°
Arg. of periapsis
89.9055°
True anomaly
270.21631°
Mean anomaly
270.2348°
Eccentric anomaly
270.22555°
Mean motion
3.73227 °/min
Orbital period
96.46 mins
BSTAR
0.0011287
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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 AJ 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-27 06:40:20.197Z | 101.64° ESE | 2025-09-27 06:42:20.197Z | 66.571° ENE | 18.401° | 2025-09-27 06:44:20.197Z | 32.016° NE |
| 6 mins | 2025-09-27 08:15:20.197Z | 211.124° SW | 2025-09-27 08:17:20.197Z | 254.065° W | 28.196° | 2025-09-27 08:21:20.197Z | 327.445° NNW |
| 6 mins | 2025-09-27 19:58:20.197Z | 39.933° NE | 2025-09-27 20:01:20.197Z | 112.731° SE | 29.967° | 2025-09-27 20:04:20.197Z | 163.137° S |
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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