OBJECT E, 64532
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 E, 64532 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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64532 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Amateur 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
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 OBJECT E
1 64532U 25135E 26035.82169837 .00014964 00000-0 64071-3 0 9991
2 64532 97.4596 152.4928 0003808 271.5188 88.5612 15.22883789 34756Epoch: 2026-02-04T19:43Z
TLE epoch observation values (Epoch: 2026-02-04T19:43:14.739Z)
Latitude
-0.00003°
Longitude
81.69862°
Altitude
500.175 km
Speed
7.614 km/s
True Right ascension
10h 09m 58s
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
09:13:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.729 km
Perigee altitude
491.495 km
Semi-major axis
6,872.249 km
Eccentricity
0.00038
Inclination
97.4596°
RAAN
152.4928°
Arg. of periapsis
271.5188°
True anomaly
88.60482°
Mean anomaly
88.5612°
Eccentric anomaly
88.58301°
Mean motion
3.80974 °/min
Orbital period
94.49 mins
BSTAR
0.00064071
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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 E 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 | 2026-02-05 08:28:08.913Z | 218.818° SW | 2026-02-05 08:30:08.913Z | 258.14° W | 20.727° | 2026-02-05 08:33:08.913Z | 316.142° NNW |
| 4 mins | 2026-02-05 19:58:08.913Z | 59.481° ENE | 2026-02-05 19:59:08.913Z | 85.512° E | 25.199° | 2026-02-05 20:02:08.913Z | 153.325° SSE |
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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