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.

Loading next visibility...
Identifier
64532, 2025-135E
Orbit
SSO
Country
Flag of TBDTBD
Related business
None
Manufacturer
Unknown
Mission
Operational Amateur Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2025-06-23 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 OBJECT E
1 64532U 25135E   26178.29250140  .00011783  00000-0  45488-3 0  9995
2 64532  97.4741 294.5256 0005630 126.6033 233.5724 15.26420364 56462
Epoch: 2026-06-27T07:01Z
TLE epoch observation values (Epoch: 2026-06-27T07:01:12.120Z)
Latitude
-0.00006°
Longitude
-86.18364°
Altitude
491.918 km
Speed
7.618 km/s
True Right ascension
19h 38m 06s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
04:25:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.347 km
Perigee altitude
479.621 km
Semi-major axis
6,861.621 km
Eccentricity
0.00056
Inclination
97.4741°
RAAN
294.5256°
Arg. of periapsis
126.6033°
True anomaly
233.52051°
Mean anomaly
233.5724°
Eccentric anomaly
233.54645°
Mean motion
3.81859 °/min
Orbital period
94.28 mins
BSTAR
0.00045488
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|