IUS R/B(2), 19550

Orbit data source: Space-Track

IUS R/B(2), 19550 is space debris in GEO originally from a launch on Thu, 29 Sep 1988 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
19550, 1988-091D
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
UTC CSD
Mission
Spacecraft
Bus & Motor
ORBUS 6, Unknown motor
Mass
~1,080 kg wet, ~1,080 kg dry
Launch date (UTC)
1988-09-29 (37 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.4 m
Radar Cross Section
8.086 m², Large (>1 m²)

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

TLE from 15 hours ago
0 IUS R/B(2)
1 19550U 88091D   26061.43496782 -.00000301  00000-0  00000-0 0  9999
2 19550  12.3397 331.7612 0020618 304.1619 330.0320  1.00479579129039
Epoch: 2026-03-02T10:26Z
TLE epoch observation values (Epoch: 2026-03-02T10:26:21.219Z)
Latitude
-12.30774°
Longitude
-70.85427°
Altitude
35,655.756 km
Speed
3.082 km/s
True Right ascension
16h 23m 51s
True Declination
-12° 17' 44"
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
05:23:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,816.261 km
Perigee altitude
35,642.626 km
Semi-major axis
42,107.58 km
Eccentricity
0.00206
Inclination
12.3397°
RAAN
331.7612°
Arg. of periapsis
304.1619°
True anomaly
329.91372°
Mean anomaly
330.032°
Eccentric anomaly
329.97289°
Mean motion
0.25119 °/min
Orbital period
1,433.18 mins
BSTAR
0
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Other satellites on launch #91 in the year 1988 (1988-09-29 UTC)

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