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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https://www.satcat.com/sats-embedded/41080?theme=dark&initialShowStats=false

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Identifier

41080, 2000-055AP

Orbit

SSO

Country

Related business

National Oceanic and Atmospheric Administration (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2000-09-21 (25 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: 2 days ago

TLE from 2 days ago

0 NOAA 16 DEB
1 41080U 00055AP  26037.06624401  .00004158  00000-0  18496-2 0  9992
2 41080  98.5358  83.8750 0007158 244.3831 115.6608 14.23395055526232

Epoch: 2026-02-06T01:35Z

TLE epoch observation values (Epoch: 2026-02-06T01:35:23.482Z)

Latitude

-0.00008°

Longitude

-76.18229°

Altitude

819.051 km

Speed

7.442 km/s

True Right ascension

05h 35m 30s

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

16:02:25

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

816.186 km

Perigee altitude

805.894 km

Semi-major axis

7,189.177 km

Eccentricity

0.00072

Inclination

98.5358°

RAAN

83.875°

Arg. of periapsis

244.3831°

True anomaly

115.73471°

Mean anomaly

115.6608°

Eccentric anomaly

115.69776°

Mean motion

3.56061 °/min

Orbital period

101.11 mins

BSTAR

0.0018496

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Other satellites on launch #55 in the year 2000 (2000-09-21 UTC)

NOAA 16 DEB, 42389 (Decayed)

NOAA 16 DEB, 42332 (Decayed)

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NOAA 16 DEB Visibility forecast

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Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
9 mins	2026-02-07 15:17:06.375Z	29.226° NE	2026-02-07 15:22:06.375Z	102.521° ESE	32.738°	2026-02-07 15:26:06.375Z	163.544° S
6 mins	2026-02-07 16:59:06.375Z	333.702° NNW	2026-02-07 17:02:06.375Z	286.666° WNW	22.993°	2026-02-07 17:05:06.375Z	246.738° WSW
8 mins	2026-02-08 02:39:06.375Z	145.731° SSE	2026-02-08 02:42:06.375Z	94.449° ESE	40.339°	2026-02-08 02:47:06.375Z	355.753° N
4 mins	2026-02-08 04:21:06.375Z	245.97° WSW	2026-02-08 04:23:06.375Z	271.945° WNW	15.684°	2026-02-08 04:25:06.375Z	296.773° NW

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out NOAA 16 DEB, 41080 on other resources

View NOAA 16 DEB, 41080 on Heavens-Above

View NOAA 16 DEB, 41080 on Keep Track

View NOAA 16 DEB, 41080 on Celestrak

View NOAA 16 DEB, 41080 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

NOAA 16 DEB, 41080

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-02-06T01:35:23.482Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #55 in the year 2000 (2000-09-21 UTC)

NOAA 16 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out NOAA 16 DEB, 41080 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago