OBJECT AL, 69014

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 AL, 69014 is a satellite in SSO that was launched on Sun, 03 May 2026 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
69014, 2026-100AL
Orbit
SSO
Country
Flag of TBDTBD
Related business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-05-03 (2 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Unknown
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 OBJECT AL
1 69014U 26100AL  26175.17395469  .00003710  00000-0  16927-3 0  9993
2 69014  97.4063  72.9489 0007204  45.6538 314.5287 15.21214850  7875
Epoch: 2026-06-24T04:10Z
TLE epoch observation values (Epoch: 2026-06-24T04:10:29.685Z)
Latitude
-0.00001°
Longitude
97.99025°
Altitude
501.792 km
Speed
7.615 km/s
True Right ascension
04h 51m 47s
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
08:51:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.094 km
Perigee altitude
494.185 km
Semi-major axis
6,877.276 km
Eccentricity
0.00072
Inclination
97.4063°
RAAN
72.9489°
Arg. of periapsis
45.6538°
True anomaly
314.46981°
Mean anomaly
314.5287°
Eccentric anomaly
314.49926°
Mean motion
3.80556 °/min
Orbital period
94.6 mins
BSTAR
0.00016927
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
|