NOAA 16 DEB, 41256

Orbit data source: Space-Track

NOAA 16 DEB, 41256 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/41256?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41256, 2000-055FG

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)

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

TLE from 3 days ago

0 NOAA 16 DEB
1 41256U 00055FG  26170.54462133  .00007958  00000-0  17568-2 0  9990
2 41256  99.0855  79.1244 0013439 127.1167 233.1259 14.57559656544526

Epoch: 2026-06-19T13:04Z

TLE epoch observation values (Epoch: 2026-06-19T13:04:15.282Z)

Latitude

-0.00005°

Longitude

-24.71134°

Altitude

709.736 km

Speed

7.498 km/s

True Right ascension

05h 16m 29s

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

21:36:27

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

707.702 km

Perigee altitude

688.682 km

Semi-major axis

7,076.329 km

Eccentricity

0.00134

Inclination

99.0855°

RAAN

79.1244°

Arg. of periapsis

127.1167°

True anomaly

233.00283°

Mean anomaly

233.1259°

Eccentric anomaly

233.06435°

Mean motion

3.64612 °/min

Orbital period

98.74 mins

BSTAR

0.0017568

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

NOAA 16 DEB, 41047 (Decayed)

NOAA 16 DEB, 42360 (Decayed)

NOAA 16 DEB, 41127 (Decayed)

NOAA 16 DEB, 41217

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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	2026-06-22 17:00:25.234Z	115.065° SE	2026-06-22 17:03:25.234Z	66.053° ENE	23.946°	2026-06-22 17:06:25.234Z	17.617° NNE
6 mins	2026-06-22 18:38:25.234Z	214.54° SW	2026-06-22 18:40:25.234Z	250.897° W	26.891°	2026-06-22 18:44:25.234Z	320.385° NNW
7 mins	2026-06-23 06:37:25.234Z	27.057° NE	2026-06-23 06:40:25.234Z	90.891° ESE	40.473°	2026-06-23 06:44:25.234Z	179.628° S

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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, 41256 on other resources

View NOAA 16 DEB, 41256 on Heavens-Above

View NOAA 16 DEB, 41256 on Keep Track

View NOAA 16 DEB, 41256 on Celestrak

View NOAA 16 DEB, 41256 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, 41256

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: 2026-06-19T13:04:15.282Z)

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, 41256 on other resources

Documentation

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