NOAA 16 DEB, 41206

Orbit data source: Space-Track

NOAA 16 DEB, 41206 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/41206?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41206, 2000-055DK

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: 6 hours ago

TLE from 6 hours ago

0 NOAA 16 DEB
1 41206U 00055DK  26062.08164546  .00003393  00000-0  14514-2 0  9998
2 41206  98.6203 105.4635 0013557 113.6821 246.5783 14.25531180527469

Epoch: 2026-03-03T01:57Z

TLE epoch observation values (Epoch: 2026-03-03T01:57:34.167Z)

Latitude

-0.00004°

Longitude

-84.79468°

Altitude

813.516 km

Speed

7.444 km/s

True Right ascension

07h 01m 51s

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

11:30:20

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

813.591 km

Perigee altitude

794.118 km

Semi-major axis

7,181.991 km

Eccentricity

0.00136

Inclination

98.6203°

RAAN

105.4635°

Arg. of periapsis

113.6821°

True anomaly

246.43584°

Mean anomaly

246.5783°

Eccentric anomaly

246.50706°

Mean motion

3.56596 °/min

Orbital period

100.95 mins

BSTAR

0.0014514

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

NOAA 16 DEB, 41093 (Decayed)

NOAA 16 DEB, 41225 (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.
5 mins	2026-03-03 14:22:23.352Z	62.247° ENE	2026-03-03 14:24:23.352Z	86.261° E	14.384°	2026-03-03 14:27:23.352Z	122.708° SE
8 mins	2026-03-03 16:01:23.352Z	2.782° NNE	2026-03-03 16:05:23.352Z	262.283° W	41.099°	2026-03-03 16:09:23.352Z	208.635° SW
6 mins	2026-03-04 01:42:23.352Z	104.546° ESE	2026-03-04 01:45:23.352Z	59.561° ENE	21.785°	2026-03-04 01:48:23.352Z	19.587° NNE
8 mins	2026-03-04 03:21:23.352Z	200.152° SSW	2026-03-04 03:24:23.352Z	254.506° W	33.909°	2026-03-04 03:29:23.352Z	331.608° NNW

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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, 41206 on other resources

View NOAA 16 DEB, 41206 on Heavens-Above

View NOAA 16 DEB, 41206 on Keep Track

View NOAA 16 DEB, 41206 on Celestrak

View NOAA 16 DEB, 41206 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, 41206

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 hours ago

TLE from 6 hours ago

TLE epoch observation values (Epoch: 2026-03-03T01:57:34.167Z)

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, 41206 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 6 hours ago