NOAA 16 DEB, 41532

Orbit data source: Space-Track

NOAA 16 DEB, 41532 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/41532?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41532, 2000-055NG

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: 23 hours ago

TLE from 23 hours ago

0 NOAA 16 DEB
1 41532U 00055NG  26022.71183499  .00006636  00000-0  24369-2 0  9996
2 41532  98.7352 122.1136 0011650 224.8545 135.1698 14.33007546505455

Epoch: 2026-01-22T17:05Z

TLE epoch observation values (Epoch: 2026-01-22T17:05:02.543Z)

Latitude

0.00002°

Longitude

103.79193°

Altitude

790.548 km

Speed

7.455 km/s

True Right ascension

08h 08m 27s

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

17:12:04

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

787.176 km

Perigee altitude

770.5 km

Semi-major axis

7,156.975 km

Eccentricity

0.00117

Inclination

98.7352°

RAAN

122.1136°

Arg. of periapsis

224.8545°

True anomaly

135.26382°

Mean anomaly

135.1698°

Eccentric anomaly

135.21682°

Mean motion

3.58467 °/min

Orbital period

100.43 mins

BSTAR

0.0024369

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

NOAA 16 DEB, 42336 (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	2026-01-23 18:48:31.756Z	33.148° NE	2026-01-23 18:52:31.756Z	96.078° ESE	32.258°	2026-01-23 18:56:31.756Z	162.763° S
6 mins	2026-01-23 20:29:31.756Z	329.081° NNW	2026-01-23 20:31:31.756Z	296.943° NW	22.62°	2026-01-23 20:35:31.756Z	242.947° WSW
8 mins	2026-01-24 06:05:31.756Z	141.299° SSE	2026-01-24 06:08:31.756Z	78.393° E	39.433°	2026-01-24 06:13:31.756Z	355.938° N
5 mins	2026-01-24 07:46:31.756Z	244.225° WSW	2026-01-24 07:48:31.756Z	271.514° WNW	16.28°	2026-01-24 07:51:31.756Z	307.426° 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, 41532 on other resources

View NOAA 16 DEB, 41532 on Heavens-Above

View NOAA 16 DEB, 41532 on Keep Track

View NOAA 16 DEB, 41532 on Celestrak

View NOAA 16 DEB, 41532 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, 41532

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: 2026-01-22T17:05:02.543Z)

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, 41532 on other resources

Documentation

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