ATLAS H R/B, 16592

Orbit data source: Space-Track

ATLAS H R/B, 16592 is space debris in LEO originally from a launch on Sun, 09 Feb 1986 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
16592, 1986-014B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
MSD-PS, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
1986-02-09 (40 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 ATLAS H R/B
1 16592U 86014B   26171.43142441  .00000551  00000-0  49891-3 0  9997
2 16592  63.3370 187.3236 0294770 137.4703 224.9585 13.74566621360691
Epoch: 2026-06-20T10:21Z
TLE epoch observation values (Epoch: 2026-06-20T10:21:15.069Z)
Latitude
Longitude
123.36467°
Altitude
1,141.666 km
Speed
7.205 km/s
True Right ascension
12h 29m 17s
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
23:08:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,198.996 km
Perigee altitude
765.085 km
Semi-major axis
7,360.178 km
Eccentricity
0.02948
Inclination
63.337°
RAAN
187.3236°
Arg. of periapsis
137.4703°
True anomaly
222.6331°
Mean anomaly
224.9585°
Eccentric anomaly
223.78975°
Mean motion
3.43725 °/min
Orbital period
104.73 mins
BSTAR
0.00049891
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