IUS R/B(1), 16118

Orbit data source: Space-Track

IUS R/B(1), 16118 is space debris in HEO originally from a launch on Thu, 03 Oct 1985 UTC launched from the Air Force Eastern Test Range (AFETR). 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
16118, 1985-092D
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
UTC CSD
Mission
Spacecraft
Bus & Motor
ORBUS 21, Unknown motor
Mass
~1,164 kg wet, ~1,164 kg dry
Launch date (UTC)
1985-10-03 (41 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 days ago

TLE from 5 days ago
0 IUS R/B(1)
1 16118U 85092D   26257.67514912 -.00000030  00000-0  75486-3 0  9995
2 16118  25.1608 125.3644 7165957 240.9350  30.9072  2.29193451 62879
Epoch: 2026-09-14T16:12Z
TLE epoch observation values (Epoch: 2026-09-14T16:12:12.883Z)
Latitude
-0.00006°
Longitude
-111.20705°
Altitude
11,773.553 km
Speed
5.245 km/s
True Right ascension
08h 21m 59s
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
19:05:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,341.281 km
Perigee altitude
509.602 km
Semi-major axis
24,303.578 km
Eccentricity
0.7166
Inclination
25.1608°
RAAN
125.3644°
Arg. of periapsis
240.935°
True anomaly
119.1159°
Mean anomaly
30.9072°
Eccentric anomaly
69.31952°
Mean motion
0.57285 °/min
Orbital period
628.44 mins
BSTAR
0.00075486
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Other satellites on launch #92 in the year 1985 (1985-10-03 UTC)

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