NOAA 16 DEB, 41525

Orbit data source: Space-Track

NOAA 16 DEB, 41525 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/41525?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41525, 2000-055MZ

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)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 NOAA 16 DEB
1 41525U 00055MZ  26033.04273090  .00003516  00000-0  13889-2 0  9992
2 41525  98.6618 105.2752 0013325 196.1307 163.9452 14.29607917510316

Epoch: 2026-02-02T01:01Z

TLE epoch observation values (Epoch: 2026-02-02T01:01:31.949Z)

Latitude

-0.00008°

Longitude

-42.3516°

Altitude

805.157 km

Speed

7.446 km/s

True Right ascension

07h 01m 06s

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

13:43:43

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

799.737 km

Perigee altitude

780.633 km

Semi-major axis

7,168.322 km

Eccentricity

0.00133

Inclination

98.6618°

RAAN

105.2752°

Arg. of periapsis

196.1307°

True anomaly

163.98736°

Mean anomaly

163.9452°

Eccentric anomaly

163.96629°

Mean motion

3.57616 °/min

Orbital period

100.67 mins

BSTAR

0.0013889

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

NOAA 16 DEB, 41497

NOAA 16 DEB, 41048 (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	2026-02-03 16:16:30.380Z	58.483° ENE	2026-02-03 16:19:30.380Z	94.815° ESE	14.349°	2026-02-03 16:21:30.380Z	119.307° SE
8 mins	2026-02-03 17:55:30.380Z	2.957° NNE	2026-02-03 17:59:30.380Z	266.402° W	41.123°	2026-02-03 18:03:30.380Z	209.015° SW
6 mins	2026-02-04 03:35:30.380Z	96.7° ESE	2026-02-04 03:37:30.380Z	65.948° ENE	21.436°	2026-02-04 03:41:30.380Z	14.904° NNE
8 mins	2026-02-04 05:13:30.380Z	198.24° SSW	2026-02-04 05:16:30.380Z	251.578° W	34.475°	2026-02-04 05:21:30.380Z	331.815° 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, 41525 on other resources

View NOAA 16 DEB, 41525 on Heavens-Above

View NOAA 16 DEB, 41525 on Keep Track

View NOAA 16 DEB, 41525 on Celestrak

View NOAA 16 DEB, 41525 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, 41525

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: 2026-02-02T01:01:31.949Z)

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, 41525 on other resources

Documentation

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