NOAA 16 DEB, 41654

Orbit data source: Space-Track

NOAA 16 DEB, 41654 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/41654?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41654, 2000-055NT

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

Small (<0.1 m²)

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

TLE from 23 hours ago

0 NOAA 16 DEB
1 41654U 00055NT  26127.85219127  .00002653  00000-0  10621-2 0  9991
2 41654  98.6239 179.1707 0034977 266.6575  93.0605 14.28855035519535

Epoch: 2026-05-07T20:27Z

TLE epoch observation values (Epoch: 2026-05-07T20:27:09.325Z)

Latitude

-0.00005°

Longitude

6.68947°

Altitude

799.917 km

Speed

7.453 km/s

True Right ascension

11h 56m 40s

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

03:19:43

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

817.785 km

Perigee altitude

767.622 km

Semi-major axis

7,170.84 km

Eccentricity

0.0035

Inclination

98.6239°

RAAN

179.1707°

Arg. of periapsis

266.6575°

True anomaly

93.46064°

Mean anomaly

93.0605°

Eccentric anomaly

93.26058°

Mean motion

3.57428 °/min

Orbital period

100.72 mins

BSTAR

0.0010621

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

NOAA 16 DEB, 41662 (Decayed)

NOAA 16 DEB, 41093 (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	2026-05-09 02:49:40.864Z	140.294° SSE	2026-05-09 02:53:40.864Z	83.525° E	35.733°	2026-05-09 02:58:40.864Z	0.232° NNE
6 mins	2026-05-09 04:31:40.864Z	235.49° WSW	2026-05-09 04:33:40.864Z	264.214° W	19.785°	2026-05-09 04:37:40.864Z	314.299° NW
5 mins	2026-05-09 15:05:40.864Z	62.529° ENE	2026-05-09 15:07:40.864Z	88.718° E	17.143°	2026-05-09 15:10:40.864Z	127.533° SE
9 mins	2026-05-09 16:43:40.864Z	0.85° NNE	2026-05-09 16:47:40.864Z	294.098° NW	38.964°	2026-05-09 16:52:40.864Z	212.883° SW

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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, 41654 on other resources

View NOAA 16 DEB, 41654 on Heavens-Above

View NOAA 16 DEB, 41654 on Keep Track

View NOAA 16 DEB, 41654 on Celestrak

View NOAA 16 DEB, 41654 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, 41654

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: 2026-05-07T20:27:09.325Z)

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, 41654 on other resources

Documentation

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