NOAA 16 DEB, 41258

Orbit data source: Space-Track

NOAA 16 DEB, 41258 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/41258?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41258, 2000-055FJ

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: 22 hours ago

TLE from 22 hours ago

0 NOAA 16 DEB
1 41258U 00055FJ  26040.15469592  .00010367  00000-0  21412-2 0  9992
2 41258  98.9877 294.4992 0039929  79.9521 280.6178 14.60079086527865

Epoch: 2026-02-09T03:42Z

TLE epoch observation values (Epoch: 2026-02-09T03:42:45.727Z)

Latitude

-0.00007°

Longitude

99.5551°

Altitude

690.784 km

Speed

7.514 km/s

True Right ascension

19h 37m 59s

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

04:21:37

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

718.26 km

Perigee altitude

661.815 km

Semi-major axis

7,068.175 km

Eccentricity

0.00399

Inclination

98.9877°

RAAN

294.4992°

Arg. of periapsis

79.9521°

True anomaly

280.16767°

Mean anomaly

280.6178°

Eccentric anomaly

280.39278°

Mean motion

3.65243 °/min

Orbital period

98.56 mins

BSTAR

0.0021412

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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	2026-02-10 04:58:25.382Z	46.674° ENE	2026-02-10 05:01:25.382Z	96.227° ESE	23.794°	2026-02-10 05:04:25.382Z	146.256° SSE
6 mins	2026-02-10 06:36:25.382Z	338.686° N	2026-02-10 06:38:25.382Z	302.872° NW	25.872°	2026-02-10 06:42:25.382Z	235.174° WSW
5 mins	2026-02-10 16:03:25.382Z	110.424° ESE	2026-02-10 16:05:25.382Z	70.369° E	26.192°	2026-02-10 16:08:25.382Z	16.121° NNE
6 mins	2026-02-10 17:40:25.382Z	218.88° SW	2026-02-10 17:43:25.382Z	273.732° WNW	22.935°	2026-02-10 17:46:25.382Z	317.344° 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, 41258 on other resources

View NOAA 16 DEB, 41258 on Heavens-Above

View NOAA 16 DEB, 41258 on Keep Track

View NOAA 16 DEB, 41258 on Celestrak

View NOAA 16 DEB, 41258 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, 41258

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 22 hours ago

TLE from 22 hours ago

TLE epoch observation values (Epoch: 2026-02-09T03:42:45.727Z)

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, 41258 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 22 hours ago