OBJECT E, 100469

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 E, 100469 is a satellite owned by Harbin (CN) in SSO that was launched on Tue, 25 Aug 2026 UTC via a CHANG ZHENG 6C launch vehicle from the Taiyaun Space Center, China (TSC). 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
100469, 2026-195E
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Harbin
Mission
Operational Commercial Imaging
Bus & Motor
BY04, Unknown motor
Mass
19 kg wet, 19 kg dry
Launch date (UTC)
2026-08-25 (2 months ago)
Launch vehicle
CHANG ZHENG 6C
Launch site
Taiyaun Space Center, China (TSC)
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.4 m
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 OBJECT E
1 A0469U 26195E   26296.23499721  .00004590  00000-0  28528-3 0  9990
2 A0469  97.5316   9.0412 0013559  72.9671 287.3043 15.10068013  8924
Epoch: 2026-10-23T05:38Z
TLE epoch observation values (Epoch: 2026-10-23T05:38:23.758Z)
Latitude
-0.00004°
Longitude
-107.21624°
Altitude
536.288 km
Speed
7.596 km/s
True Right ascension
00h 36m 09s
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
07:18:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
542.348 km
Perigee altitude
523.606 km
Semi-major axis
6,911.114 km
Eccentricity
0.00136
Inclination
97.5316°
RAAN
9.0412°
Arg. of periapsis
72.9671°
True anomaly
287.15588°
Mean anomaly
287.3043°
Eccentric anomaly
287.2301°
Mean motion
3.77764 °/min
Orbital period
95.3 mins
BSTAR
0.00028528
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
|