OBJECT W, 69000

Orbit data source: Space-Track

You're viewing an uncataloged RSO

Recently launched and/or uncataloged RSOs may have evolving metadata. Metadata may include the following, but is not limited to: Owner, Manufacturer, Bus, Motor, and Mission.

OBJECT W, 69000 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
69000, 2026-100W
Orbit
SSO
Country
Flag of TBDTBD
Related business
Manufacturer
NCKU
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2026-05-03 (3 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Unknown
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.035 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 W
1 69000U 26100W   26220.69627578  .00000740  00000-0  77682-4 0  9991
2 69000  97.7254 117.1892 0002536  82.0858 278.0649 14.92402496 14537
Epoch: 2026-08-08T16:42Z
TLE epoch observation values (Epoch: 2026-08-08T16:42:38.227Z)
Latitude
-0.00002°
Longitude
-90.67399°
Altitude
593.243 km
Speed
7.563 km/s
True Right ascension
07h 48m 45s
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
22:29:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.23 km
Perigee altitude
585.697 km
Semi-major axis
6,965.6 km
Eccentricity
0.00025
Inclination
97.7254°
RAAN
117.1892°
Arg. of periapsis
82.0858°
True anomaly
278.03613°
Mean anomaly
278.0649°
Eccentric anomaly
278.05051°
Mean motion
3.73341 °/min
Orbital period
96.43 mins
BSTAR
0.000077682
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
|