NOAA 16 DEB, 41520

Orbit data source: Space-Track

NOAA 16 DEB, 41520 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/41520?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41520, 2000-055MU

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: 3 days ago

TLE from 3 days ago

0 NOAA 16 DEB
1 41520U 00055MU  26125.86417709  .00042718  00000-0  54910-2 0  9993
2 41520  98.8625 275.3146 0018778 103.3661 256.9644 14.80862547520548

Epoch: 2026-05-05T20:44Z

TLE epoch observation values (Epoch: 2026-05-05T20:44:24.900Z)

Latitude

0.00004°

Longitude

100.47794°

Altitude

632.586 km

Speed

7.54 km/s

True Right ascension

18h 21m 15s

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

01:20:16

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

636.836 km

Perigee altitude

610.54 km

Semi-major axis

7,001.825 km

Eccentricity

0.00188

Inclination

98.8625°

RAAN

275.3146°

Arg. of periapsis

103.3661°

True anomaly

256.75488°

Mean anomaly

256.9644°

Eccentric anomaly

256.85963°

Mean motion

3.70447 °/min

Orbital period

97.18 mins

BSTAR

0.005491

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

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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	2026-05-08 22:17:33.438Z	41.565° NE	2026-05-08 22:20:33.438Z	102.829° ESE	28.417°	2026-05-08 22:23:33.438Z	158.024° S
4 mins	2026-05-08 23:54:33.438Z	325.871° NNW	2026-05-08 23:56:33.438Z	289.142° WNW	19.55°	2026-05-08 23:58:33.438Z	255.581° W
6 mins	2026-05-09 09:12:33.438Z	117.386° SE	2026-05-09 09:14:33.438Z	80.434° E	25.548°	2026-05-09 09:18:33.438Z	9.626° NNE
4 mins	2026-05-09 10:49:33.438Z	233.331° WSW	2026-05-09 10:51:33.438Z	273.479° WNW	20.928°	2026-05-09 10:53:33.438Z	307.006° 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, 41520 on other resources

View NOAA 16 DEB, 41520 on Heavens-Above

View NOAA 16 DEB, 41520 on Keep Track

View NOAA 16 DEB, 41520 on Celestrak

View NOAA 16 DEB, 41520 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, 41520

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-05-05T20:44:24.900Z)

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, 41520 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago