NOAA 16 DEB, 42396

Orbit data source: Space-Track

NOAA 16 DEB, 42396 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/42396?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

42396, 2000-055SQ

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

Medium (>0.1 m² and <1 m²)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 NOAA 16 DEB
1 42396U 00055SQ  26184.88697299  .00011424  00000-0  23530-2 0  9990
2 42396  98.8031 340.3144 0023024 322.1006  37.8571 14.60510473539750

Epoch: 2026-07-03T21:17Z

TLE epoch observation values (Epoch: 2026-07-03T21:17:14.466Z)

Latitude

-0.00001°

Longitude

99.09556°

Altitude

681.653 km

Speed

7.523 km/s

True Right ascension

22h 41m 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

19:56:33

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

704.906 km

Perigee altitude

672.365 km

Semi-major axis

7,066.772 km

Eccentricity

0.0023

Inclination

98.8031°

RAAN

340.3144°

Arg. of periapsis

322.1006°

True anomaly

38.01938°

Mean anomaly

37.8571°

Eccentric anomaly

37.9382°

Mean motion

3.65352 °/min

Orbital period

98.54 mins

BSTAR

0.002353

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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.
7 mins	2026-07-05 09:35:41.222Z	126.574° SE	2026-07-05 09:39:41.222Z	60.079° ENE	26.845°	2026-07-05 09:42:41.222Z	12.562° NNE
5 mins	2026-07-05 11:14:41.222Z	225.212° WSW	2026-07-05 11:16:41.222Z	261.725° W	23.475°	2026-07-05 11:19:41.222Z	311.842° NW
8 mins	2026-07-05 23:11:41.222Z	20.081° NNE	2026-07-05 23:14:41.222Z	58.581° ENE	42.563°	2026-07-05 23:19:41.222Z	187.772° 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, 42396 on other resources

View NOAA 16 DEB, 42396 on Heavens-Above

View NOAA 16 DEB, 42396 on Keep Track

View NOAA 16 DEB, 42396 on Celestrak

View NOAA 16 DEB, 42396 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, 42396

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-07-03T21:17:14.466Z)

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, 42396 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago