OBJECT H, 55016

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 H, 55016 is a satellite in SSO that was launched on Tue, 03 Jan 2023 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
55016, 2023-001H
Orbit
SSO
Country
Flag of TBDTBD
Related business
None
Manufacturer
Unknown
Mission
Non-operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2023-01-03 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 OBJECT H
1 55016U 23001H   26235.93664440  .00012015  00000-0  27352-3 0  9998
2 55016  97.3105 300.3060 0005275 208.3555 151.7406 15.43094535202662
Epoch: 2026-08-23T22:28Z
TLE epoch observation values (Epoch: 2026-08-23T22:28:46.076Z)
Latitude
-0.00006°
Longitude
-9.11152°
Altitude
443.275 km
Speed
7.644 km/s
True Right ascension
20h 01m 13s
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
04:19:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
437.507 km
Perigee altitude
430.32 km
Semi-major axis
6,812.051 km
Eccentricity
0.00053
Inclination
97.3105°
RAAN
300.306°
Arg. of periapsis
208.3555°
True anomaly
151.7692°
Mean anomaly
151.7406°
Eccentric anomaly
151.7549°
Mean motion
3.86035 °/min
Orbital period
93.26 mins
BSTAR
0.00027352
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|