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)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 NIMBUS 2 DEB
1 28201U 66040P   26060.61290602  .00002366  00000-0  31129-2 0  9994
2 28201 100.2663 339.0278 0055020 247.3885 233.0061 13.61785913636570

Epoch: 2026-03-01T14:42Z

TLE epoch observation values (Epoch: 2026-03-01T14:42:35.080Z)

Latitude

58.64404°

Longitude

156.16377°

Altitude

1,063.688 km

Speed

7.313 km/s

True Right ascension

11h 44m 54s

True Declination

58° 29' 50"

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

06:20:07

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,067.265 km

Perigee altitude

985.784 km

Semi-major axis

7,404.661 km

Eccentricity

0.0055

Inclination

100.2663°

RAAN

339.0278°

Arg. of periapsis

247.3885°

True anomaly

232.50462°

Mean anomaly

233.0061°

Eccentric anomaly

232.75515°

Mean motion

3.40632 °/min

Orbital period

105.69 mins

BSTAR

0.0031129

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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	2026-03-02 06:35:57.305Z	36.02° NE	2026-03-02 06:40:57.305Z	94.721° ESE	30.282°	2026-03-02 06:45:57.305Z	158.666° S
10 mins	2026-03-02 08:20:57.305Z	352.626° N	2026-03-02 08:24:57.305Z	301.35° NW	31.468°	2026-03-02 08:30:57.305Z	230.2° WSW
6 mins	2026-03-02 16:45:57.305Z	82.862° E	2026-03-02 16:47:57.305Z	61.407° ENE	17.658°	2026-03-02 16:51:57.305Z	20.603° NNE
11 mins	2026-03-02 18:26:57.305Z	168.58° S	2026-03-02 18:31:57.305Z	284.691° WNW	44.478°	2026-03-02 18:37:57.305Z	342.216° N

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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: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-03-01T14:42:35.080Z)

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: 12 hours ago