NOAA 16 DEB, 41055

Orbit data source: Space-Track

NOAA 16 DEB, 41055 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/41055?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41055, 2000-055N

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, 0.2 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago

0 NOAA 16 DEB
1 41055U 00055N   26037.85326076  .00006377  00000-0  22437-2 0  9993
2 41055  98.7831 150.4253 0016265 223.0031 136.9883 14.35139271528889

Epoch: 2026-02-06T20:28Z

TLE epoch observation values (Epoch: 2026-02-06T20:28:41.729Z)

Latitude

-0.00006°

Longitude

66.26626°

Altitude

786.054 km

Speed

7.456 km/s

True Right ascension

10h 01m 42s

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

06:18:42

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

783.375 km

Perigee altitude

760.116 km

Semi-major axis

7,149.883 km

Eccentricity

0.00163

Inclination

98.7831°

RAAN

150.4253°

Arg. of periapsis

223.0031°

True anomaly

137.11525°

Mean anomaly

136.9883°

Eccentric anomaly

137.05179°

Mean motion

3.59 °/min

Orbital period

100.28 mins

BSTAR

0.0022437

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

NOAA 16 DEB, 41200 (Decayed)

NOAA 16 DEB, 41407 (Decayed)

NOAA 16 DEB, 41527

NOAA 16 DEB, 41371 (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.
8 mins	2026-02-07 06:38:58.776Z	131.235° SE	2026-02-07 06:42:58.776Z	70.555° E	30.969°	2026-02-07 06:46:58.776Z	7.261° NNE
6 mins	2026-02-07 08:19:58.776Z	227.591° WSW	2026-02-07 08:21:58.776Z	259.981° W	23.384°	2026-02-07 08:25:58.776Z	316.757° NNW
8 mins	2026-02-07 20:29:58.776Z	6.833° NNE	2026-02-07 20:32:58.776Z	296.371° NW	43.916°	2026-02-07 20:37:58.776Z	201.842° SSW

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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, 41055 on other resources

View NOAA 16 DEB, 41055 on Heavens-Above

View NOAA 16 DEB, 41055 on Keep Track

View NOAA 16 DEB, 41055 on Celestrak

View NOAA 16 DEB, 41055 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, 41055

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-02-06T20:28:41.729Z)

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, 41055 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago