NOAA 16 DEB, 41080

Orbit data source: Space-Track

NOAA 16 DEB, 41080 is space debris in SSO originally from a launch on Thu, 21 Sep 2000 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
41080, 2000-055AP
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2000-09-21 (26 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 NOAA 16 DEB
1 41080U 00055AP  26206.58494209  .00001190  00000-0  53903-3 0  9994
2 41080  98.5194 248.2124 0010572 109.0495 251.1830 14.23768242550354
Epoch: 2026-07-25T14:02Z
TLE epoch observation values (Epoch: 2026-07-25T14:02:18.996Z)
Latitude
-0.00004°
Longitude
94.33814°
Altitude
818.022 km
Speed
7.443 km/s
True Right ascension
16h 32m 50s
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
13:29:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
817.381 km
Perigee altitude
802.182 km
Semi-major axis
7,187.919 km
Eccentricity
0.00106
Inclination
98.5194°
RAAN
248.2124°
Arg. of periapsis
109.0495°
True anomaly
251.06838°
Mean anomaly
251.183°
Eccentric anomaly
251.12568°
Mean motion
3.56155 °/min
Orbital period
101.08 mins
BSTAR
0.00053903
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