NOAA 16 DEB, 41712

Orbit data source: Space-Track

NOAA 16 DEB, 41712 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/41712?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41712, 2000-055PS

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: 4 days ago

TLE from 4 days ago

0 NOAA 16 DEB
1 41712U 00055PS  26037.86224582  .00029138  00000-0  61686-2 0  9992
2 41712  98.8348 170.7974 0026545 122.4902 237.8866 14.58946076508108

Epoch: 2026-02-06T20:41Z

TLE epoch observation values (Epoch: 2026-02-06T20:41:38.038Z)

Latitude

-0.00008°

Longitude

83.39489°

Altitude

709.564 km

Speed

7.496 km/s

True Right ascension

11h 23m 11s

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

13:11:26

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

712.464 km

Perigee altitude

674.92 km

Semi-major axis

7,071.829 km

Eccentricity

0.00265

Inclination

98.8348°

RAAN

170.7974°

Arg. of periapsis

122.4902°

True anomaly

237.62941°

Mean anomaly

237.8866°

Eccentric anomaly

237.75796°

Mean motion

3.6496 °/min

Orbital period

98.64 mins

BSTAR

0.0061686

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

NOAA 16 DEB, 41518 (Decayed)

NOAA 16 DEB, 42404 (Decayed)

NOAA 16 DEB, 41225 (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.
6 mins	2026-02-10 20:44:46.840Z	49.058° ENE	2026-02-10 20:47:46.840Z	94.004° ESE	20.267°	2026-02-10 20:50:46.840Z	140.099° SSE
6 mins	2026-02-10 22:22:46.840Z	344.728° N	2026-02-10 22:25:46.840Z	280.882° WNW	29.74°	2026-02-10 22:28:46.840Z	230.79° WSW
6 mins	2026-02-11 07:49:46.840Z	110.585° ESE	2026-02-11 07:52:46.840Z	58.665° ENE	22.693°	2026-02-11 07:55:46.840Z	15.342° NNE
7 mins	2026-02-11 09:26:46.840Z	207.569° SW	2026-02-11 09:29:46.840Z	262.276° W	27.911°	2026-02-11 09:33:46.840Z	324.735° NNW

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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, 41712 on other resources

View NOAA 16 DEB, 41712 on Heavens-Above

View NOAA 16 DEB, 41712 on Keep Track

View NOAA 16 DEB, 41712 on Celestrak

View NOAA 16 DEB, 41712 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, 41712

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 4 days ago

TLE from 4 days ago

TLE epoch observation values (Epoch: 2026-02-06T20:41:38.038Z)

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, 41712 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 4 days ago