OBJECT N, 66305

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 N, 66305 is a satellite in LEO that was launched on Sun, 02 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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
66305, 2025-248N
Orbit
LEO
Country
Flag of TBDTBD
Related business
None
Manufacturer
Unknown
Mission
Operational Commercial Communications
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2025-11-02 (8 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 OBJECT N
1 66305U 25248N   26171.18520545  .00015305  00000-0  56040-3 0  9990
2 66305  45.4226  97.1260 0009519  70.8933 289.2987 15.27929581 32935
Epoch: 2026-06-20T04:26Z
TLE epoch observation values (Epoch: 2026-06-20T04:26:41.750Z)
Latitude
-0.00001°
Longitude
122.04857°
Altitude
479.896 km
Speed
7.628 km/s
True Right ascension
06h 28m 30s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
07:17:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.073 km
Perigee altitude
477.009 km
Semi-major axis
6,861.678 km
Eccentricity
0.00095
Inclination
45.4226°
RAAN
97.126°
Arg. of periapsis
70.8933°
True anomaly
289.19571°
Mean anomaly
289.2987°
Eccentric anomaly
289.24721°
Mean motion
3.81854 °/min
Orbital period
94.28 mins
BSTAR
0.0005604
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
|