NOAA 16 DEB, 42401

Orbit data source: Space-Track

NOAA 16 DEB, 42401 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
42401, 2000-055SV
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: 13 hours ago

TLE from 13 hours ago
0 NOAA 16 DEB
1 42401U 00055SV  26243.91748350  .00004490  00000-0  92389-3 0  9996
2 42401  98.9442 127.4633 0040393 169.6524 190.5514 14.60595049549485
Epoch: 2026-08-31T22:01Z
TLE epoch observation values (Epoch: 2026-08-31T22:01:10.574Z)
Latitude
-0.00008°
Longitude
177.07742°
Altitude
722.298 km
Speed
7.479 km/s
True Right ascension
08h 29m 51s
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
03:04:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
716.913 km
Perigee altitude
659.826 km
Semi-major axis
7,066.506 km
Eccentricity
0.00404
Inclination
98.9442°
RAAN
127.4633°
Arg. of periapsis
169.6524°
True anomaly
190.46706°
Mean anomaly
190.5514°
Eccentric anomaly
190.50919°
Mean motion
3.65373 °/min
Orbital period
98.53 mins
BSTAR
0.00092389
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