NOAA 16 DEB, 41706

Orbit data source: Space-Track

NOAA 16 DEB, 41706 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/41706?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41706, 2000-055PL

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: 3 days ago

TLE from 3 days ago

0 NOAA 16 DEB
1 41706U 00055PL  25339.36231192  .00004841  00000-0  24777-2 0  9993
2 41706  98.6892   8.0437 0033784  37.9879 322.3669 14.15644012501726

Epoch: 2025-12-05T08:41Z

TLE epoch observation values (Epoch: 2025-12-05T08:41:43.749Z)

Latitude

-0.00003°

Longitude

163.20593°

Altitude

823.746 km

Speed

7.451 km/s

True Right ascension

00h 32m 10s

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

01:32:36

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

861.662 km

Perigee altitude

812.909 km

Semi-major axis

7,215.423 km

Eccentricity

0.00338

Inclination

98.6892°

RAAN

8.0437°

Arg. of periapsis

37.9879°

True anomaly

322.12972°

Mean anomaly

322.3669°

Eccentric anomaly

322.24839°

Mean motion

3.5412 °/min

Orbital period

101.66 mins

BSTAR

0.0024777

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

NOAA 16 DEB, 41533 (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.
6 mins	2025-12-08 13:38:29.934Z	56.062° ENE	2025-12-08 13:41:29.934Z	90.891° ESE	15.737°	2025-12-08 13:44:29.934Z	125.994° SE
9 mins	2025-12-08 15:18:29.934Z	3.21° NNE	2025-12-08 15:22:29.934Z	282.595° WNW	41.626°	2025-12-08 15:27:29.934Z	208.286° SW
7 mins	2025-12-09 01:03:29.934Z	110.695° ESE	2025-12-09 01:06:29.934Z	65.246° ENE	24.317°	2025-12-09 01:10:29.934Z	12.501° NNE
8 mins	2025-12-09 02:43:29.934Z	204.987° SW	2025-12-09 02:46:29.934Z	255.204° W	31.141°	2025-12-09 02:51:29.934Z	328.852° 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, 41706 on other resources

View NOAA 16 DEB, 41706 on Heavens-Above

View NOAA 16 DEB, 41706 on Keep Track

View NOAA 16 DEB, 41706 on Celestrak

View NOAA 16 DEB, 41706 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, 41706

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2025-12-05T08:41:43.749Z)

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, 41706 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago