NOAA 16 DEB, 42410

Orbit data source: Space-Track

NOAA 16 DEB, 42410 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
42410, 2000-055TE
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
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 NOAA 16 DEB
1 42410U 00055TE  26235.88339124  .00006830  00000-0  15469-2 0  9991
2 42410  98.8271  32.8012 0027243 241.4164 118.4290 14.56246367546615
Epoch: 2026-08-23T21:12Z
TLE epoch observation values (Epoch: 2026-08-23T21:12:05.003Z)
Latitude
-0.00003°
Longitude
102.6073°
Altitude
717.51 km
Speed
7.492 km/s
True Right ascension
02h 11m 12s
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
13:05:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
721.726 km
Perigee altitude
683.147 km
Semi-major axis
7,080.573 km
Eccentricity
0.00272
Inclination
98.8271°
RAAN
32.8012°
Arg. of periapsis
241.4164°
True anomaly
118.70309°
Mean anomaly
118.429°
Eccentric anomaly
118.56609°
Mean motion
3.64284 °/min
Orbital period
98.82 mins
BSTAR
0.0015469
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