NOAA 16 DEB, 42379

Orbit data source: Space-Track

NOAA 16 DEB, 42379 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/42379?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

42379, 2000-055RX

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, 0.050 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 NOAA 16 DEB
1 42379U 00055RX  26276.07537222  .00013067  00000-0  15280-2 0  9991
2 42379  98.9133 143.1452 0019334 101.8980 258.4401 14.85115086552237

Epoch: 2026-10-03T01:48Z

TLE epoch observation values (Epoch: 2026-10-03T01:48:32.159Z)

Latitude

-0.00002°

Longitude

104.22303°

Altitude

618.955 km

Speed

7.548 km/s

True Right ascension

09h 32m 34s

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

07:48:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

623.818 km

Perigee altitude

596.796 km

Semi-major axis

6,988.444 km

Eccentricity

0.00193

Inclination

98.9133°

RAAN

143.1452°

Arg. of periapsis

101.898°

True anomaly

258.22315°

Mean anomaly

258.4401°

Eccentric anomaly

258.33161°

Mean motion

3.71512 °/min

Orbital period

96.9 mins

BSTAR

0.001528

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

NOAA 16 DEB, 41355 (Decayed)

NOAA 16 DEB, 42353 (Decayed)

NOAA 16 DEB, 41136 (Decayed)

NOAA 16 DEB, 42360 (Decayed)

NOAA 16 DEB, 41666 (Decayed)

NOAA 16 DEB, 41088 (Decayed)

NOAA 16 DEB, 42395 (Decayed)

NOAA 16 DEB, 41519 (Decayed)

NOAA 16 DEB, 41662 (Decayed)

NOAA 16 DEB, 41494

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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.
7 mins	2026-10-03 14:52:36.321Z	144.656° SSE	2026-10-03 14:55:36.321Z	85.056° E	51.367°	2026-10-03 14:59:36.321Z	357.607° N
6 mins	2026-10-04 04:15:36.321Z	12.404° NNE	2026-10-04 04:18:36.321Z	211.572° SW	76.533°	2026-10-04 04:21:36.321Z	196.827° SSW

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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, 42379 on other resources

View NOAA 16 DEB, 42379 on Heavens-Above

View NOAA 16 DEB, 42379 on Keep Track

View NOAA 16 DEB, 42379 on Celestrak

View NOAA 16 DEB, 42379 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, 42379

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-10-03T01:48:32.159Z)

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, 42379 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago