NIMBUS 2 DEB, 28201

Orbit data source: Space-Track

NIMBUS 2 DEB, 28201 is space debris in SSO originally from a launch on Sun, 15 May 1966 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/28201?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28201, 1966-040P

Orbit

SSO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-05-15 (60 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 NIMBUS 2 DEB
1 28201U 66040P   26120.56921361  .00002616  00000-0  34099-2 0  9995
2 28201 100.2671  42.0451 0060455  85.6132  90.0363 13.62083663644736

Epoch: 2026-04-30T13:39Z

TLE epoch observation values (Epoch: 2026-04-30T13:39:40.055Z)

Latitude

3.50809°

Longitude

159.24723°

Altitude

1,030.824 km

Speed

7.336 km/s

True Right ascension

14h 50m 42s

True Declination

3° 29' 17"

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

03:49:45

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,070.203 km

Perigee altitude

980.686 km

Semi-major axis

7,403.581 km

Eccentricity

0.00605

Inclination

100.2671°

RAAN

42.0451°

Arg. of periapsis

85.6132°

True anomaly

90.72904°

Mean anomaly

90.0363°

Eccentric anomaly

90.38267°

Mean motion

3.40706 °/min

Orbital period

105.66 mins

BSTAR

0.0034099

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Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)

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NIMBUS 2 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.
10 mins	2026-05-02 07:43:09.147Z	17.08° NNE	2026-05-02 07:47:09.147Z	42.034° NE	44.749°	2026-05-02 07:53:09.147Z	195.668° SSW
5 mins	2026-05-02 09:29:09.147Z	321.407° NNW	2026-05-02 09:31:09.147Z	299.33° NW	15.186°	2026-05-02 09:34:09.147Z	269.743° W
9 mins	2026-05-02 17:50:09.147Z	125.455° SE	2026-05-02 17:54:09.147Z	68.109° E	32.77°	2026-05-02 17:59:09.147Z	2.257° NNE
9 mins	2026-05-02 19:34:09.147Z	207.693° SW	2026-05-02 19:38:09.147Z	257.18° W	27.444°	2026-05-02 19:43:09.147Z	320.13° 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 NIMBUS 2 DEB, 28201 on other resources

View NIMBUS 2 DEB, 28201 on Heavens-Above

View NIMBUS 2 DEB, 28201 on Keep Track

View NIMBUS 2 DEB, 28201 on Celestrak

View NIMBUS 2 DEB, 28201 on Gunter's Space Page

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

NIMBUS 2 DEB, 28201

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: 2026-04-30T13:39:40.055Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)

NIMBUS 2 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out NIMBUS 2 DEB, 28201 on other resources

Documentation

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