NOAA 16 DEB, 41082

Orbit data source: Space-Track

NOAA 16 DEB, 41082 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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Iframe URL

https://www.satcat.com/sats-embedded/41082?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41082, 2000-055AR

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 (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: 23 hours ago

TLE from 23 hours ago

0 NOAA 16 DEB
1 41082U 00055AR  26284.15299277  .00000445  00000-0  46182-3 0  9996
2 41082  98.7808  38.6995 0217175 251.6715 106.0702 13.70752799543241

Epoch: 2026-10-11T03:40Z

TLE epoch observation values (Epoch: 2026-10-11T03:40:18.575Z)

Latitude

0.00004°

Longitude

-36.12776°

Altitude

1,047.242 km

Speed

7.305 km/s

True Right ascension

02h 34m 47s

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

21:14:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,154.202 km

Perigee altitude

833.989 km

Semi-major axis

7,372.233 km

Eccentricity

0.02172

Inclination

98.7808°

RAAN

38.6995°

Arg. of periapsis

251.6715°

True anomaly

108.44307°

Mean anomaly

106.0702°

Eccentric anomaly

107.2585°

Mean motion

3.42882 °/min

Orbital period

104.99 mins

BSTAR

0.00046182

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

NOAA 16 DEB, 41521 (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	2026-10-12 06:06:45.659Z	100.599° ESE	2026-10-12 06:10:45.659Z	63.919° ENE	19.974°	2026-10-12 06:15:45.659Z	16.971° NNE
12 mins	2026-10-12 07:48:45.659Z	170.309° S	2026-10-12 07:53:45.659Z	223.663° SW	78.784°	2026-10-12 08:00:45.659Z	344.229° N
11 mins	2026-10-12 20:34:45.659Z	15.997° NNE	2026-10-12 20:39:45.659Z	66.578° ENE	81.096°	2026-10-12 20:45:45.659Z	191.759° SSW
6 mins	2026-10-12 22:19:45.659Z	332.589° NNW	2026-10-12 22:22:45.659Z	302.313° NW	17.738°	2026-10-12 22:25:45.659Z	271.258° WNW

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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, 41082 on other resources

View NOAA 16 DEB, 41082 on Heavens-Above

View NOAA 16 DEB, 41082 on Keep Track

View NOAA 16 DEB, 41082 on Celestrak

View NOAA 16 DEB, 41082 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, 41082

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 23 hours ago

TLE from 23 hours ago

TLE epoch observation values (Epoch: 2026-10-11T03:40:18.575Z)

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, 41082 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 23 hours ago