NOAA 16 DEB, 41276

Orbit data source: Space-Track

NOAA 16 DEB, 41276 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/41276?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41276, 2000-055GC

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: 2 days ago

TLE from 2 days ago

0 NOAA 16 DEB
1 41276U 00055GC  26081.58064403  .00003109  00000-0  13798-2 0  9990
2 41276  98.6521 132.7372 0012534  54.7369 305.4981 14.23685451528696

Epoch: 2026-03-22T13:56Z

TLE epoch observation values (Epoch: 2026-03-22T13:56:07.644Z)

Latitude

0.00003°

Longitude

103.62039°

Altitude

810.61 km

Speed

7.451 km/s

True Right ascension

08h 50m 56s

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

04:42:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

819.076 km

Perigee altitude

801.057 km

Semi-major axis

7,188.204 km

Eccentricity

0.00125

Inclination

98.6521°

RAAN

132.7372°

Arg. of periapsis

54.7369°

True anomaly

305.38106°

Mean anomaly

305.4981°

Eccentric anomaly

305.43959°

Mean motion

3.56133 °/min

Orbital period

101.09 mins

BSTAR

0.0013798

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

NOAA 16 DEB, 41414 (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	2026-03-25 02:46:37.225Z	141.684° SSE	2026-03-25 02:51:37.225Z	56.383° ENE	35.762°	2026-03-25 02:55:37.225Z	0.765° NNE
6 mins	2026-03-25 04:28:37.225Z	229.18° WSW	2026-03-25 04:31:37.225Z	270.655° WNW	19.176°	2026-03-25 04:34:37.225Z	309.057° NW
5 mins	2026-03-25 15:05:37.225Z	65.939° ENE	2026-03-25 15:07:37.225Z	93.998° ESE	18.306°	2026-03-25 15:10:37.225Z	132.276° SE
8 mins	2026-03-25 16:44:37.225Z	353.985° N	2026-03-25 16:47:37.225Z	293.407° NW	37.682°	2026-03-25 16:52:37.225Z	215.136° 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, 41276 on other resources

View NOAA 16 DEB, 41276 on Heavens-Above

View NOAA 16 DEB, 41276 on Keep Track

View NOAA 16 DEB, 41276 on Celestrak

View NOAA 16 DEB, 41276 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, 41276

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-03-22T13:56:07.644Z)

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, 41276 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago