NOAA 16 DEB, 41402

Orbit data source: Space-Track

NOAA 16 DEB, 41402 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/41402?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41402, 2000-055KF

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: 2 days ago

TLE from 2 days ago

0 NOAA 16 DEB
1 41402U 00055KF  26036.30273418  .00004217  00000-0  20631-2 0  9994
2 41402  98.6865  68.0632 0029638 263.5517  96.2283 14.18196190513679

Epoch: 2026-02-05T07:15Z

TLE epoch observation values (Epoch: 2026-02-05T07:15:56.233Z)

Latitude

-0.00005°

Longitude

-176.378°

Altitude

836.754 km

Speed

7.433 km/s

True Right ascension

04h 32m 15s

True Declination

0° 00' 00"

Sunlit

Object was in daylight 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

14:03:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

849.979 km

Perigee altitude

807.26 km

Semi-major axis

7,206.756 km

Eccentricity

0.00296

Inclination

98.6865°

RAAN

68.0632°

Arg. of periapsis

263.5517°

True anomaly

96.56578°

Mean anomaly

96.2283°

Eccentric anomaly

96.39706°

Mean motion

3.54759 °/min

Orbital period

101.48 mins

BSTAR

0.0020631

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

NOAA 16 DEB, 42389 (Decayed)

NOAA 16 DEB, 42332 (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 14:03:05.563Z	41.01° NE	2026-02-07 14:07:05.563Z	98.353° ESE	26.463°	2026-02-07 14:11:05.563Z	152.682° SSE
7 mins	2026-02-07 15:44:05.563Z	344.512° N	2026-02-07 15:47:05.563Z	295.981° NW	29.626°	2026-02-07 15:51:05.563Z	234.308° WSW
9 mins	2026-02-08 01:26:05.563Z	137.812° SSE	2026-02-08 01:30:05.563Z	68.058° E	36.475°	2026-02-08 01:35:05.563Z	358.793° N
6 mins	2026-02-08 03:08:05.563Z	232.445° WSW	2026-02-08 03:10:05.563Z	259.66° W	20.219°	2026-02-08 03:14:05.563Z	311.471° 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, 41402 on other resources

View NOAA 16 DEB, 41402 on Heavens-Above

View NOAA 16 DEB, 41402 on Keep Track

View NOAA 16 DEB, 41402 on Celestrak

View NOAA 16 DEB, 41402 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, 41402

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: 2026-02-05T07:15:56.233Z)

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, 41402 on other resources

Documentation

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