NOAA 16 DEB, 41080

Orbit data source: Space-Track

NOAA 16 DEB, 41080 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/41080?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41080, 2000-055AP

Orbit

SSO

Last TLE update

19 hours ago

Origin

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

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 19 hours ago

0 NOAA 16 DEB
1 41080U 00055AP  25121.89146839  .00003200  00000-0  14662-2 0  9998
2 41080  98.5599 172.0350 0005913   7.9616 352.1655 14.22018178486408

Epoch: 2025-05-01T21:23Z

Definitive object data (Epoch: 2025-05-01T21:23:42.868Z)

Latitude

-0.00004°

Longitude

-8.94954°

Altitude

817.241 km

Speed

7.447 km/s

True Right ascension

11h 28m 08s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude

-6.76812°

Longitude

170.81881°

Altitude

826.825 km

Speed

7.437 km/s

Apparent Right ascension

21h 28m 34s

Apparent Declination

-60° 02' 54"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

00:33:42

Azimuth

202.161° SSW

Elevation

-16.937°

Doppler factor

Orbital elements

Apogee altitude

819.938 km

Perigee altitude

811.431 km

Semi-major axis

7,193.821 km

Eccentricity

0.0005913

Inclination

98.5599°

RAAN

172.035°

Arg. of periapsis

7.9616°

True anomaly

352.15626°

Mean anomaly

352.1655°

Eccentric anomaly

352.16088°

Mean motion

3.55716 °/min

BSTAR

0.0014662

Orbital period

101.2 mins

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

NOAA 16 DEB, 41070 (Decayed)

NOAA 16 DEB Visibility forecast

Observer location: undefined°, undefined°

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	2025-05-03 02:14:45.691Z	117.144° SE	2025-05-03 02:18:45.691Z	62.825° ENE	23.567°	2025-05-03 02:22:45.691Z	12.335° NNE
8 mins	2025-05-03 03:54:45.691Z	200.275° SSW	2025-05-03 03:58:45.691Z	270.921° WNW	32.056°	2025-05-03 04:02:45.691Z	327.684° NNW
9 mins	2025-05-03 16:11:45.691Z	14.057° NNE	2025-05-03 16:15:45.691Z	28.565° NE	44.752°	2025-05-03 16:20:45.691Z	193.969° SSW

Authenticating...

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Check out NOAA 16 DEB, 41080 on other resources

View NOAA 16 DEB, 41080 on Heavens-Above

View NOAA 16 DEB, 41080 on Keep Track

View NOAA 16 DEB, 41080 on Celestrak

View NOAA 16 DEB, 41080 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.