NIMBUS 2 DEB, 28202

Orbit data source: Space-Track

NIMBUS 2 DEB, 28202 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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https://www.satcat.com/sats-embedded/28202?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28202, 1966-040Q

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: 4 days ago

TLE from 4 days ago

0 NIMBUS 2 DEB
1 28202U 66040Q   26122.17325802  .00002539  00000-0  31869-2 0  9999
2 28202 100.1928  10.6868 0032608   7.3835 148.3800 13.64984531626531

Epoch: 2026-05-02T04:09Z

TLE epoch observation values (Epoch: 2026-05-02T04:09:29.492Z)

Latitude

23.6614°

Longitude

-87.28585°

Altitude

1,040.943 km

Speed

7.323 km/s

True Right ascension

13h 00m 43s

True Declination

23° 32' 24"

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

06:42:45

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,039.047 km

Perigee altitude

990.832 km

Semi-major axis

7,393.077 km

Eccentricity

0.00326

Inclination

100.1928°

RAAN

10.6868°

Arg. of periapsis

7.3835°

True anomaly

148.57523°

Mean anomaly

148.38°

Eccentric anomaly

148.47768°

Mean motion

3.41433 °/min

Orbital period

105.44 mins

BSTAR

0.0031869

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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.
11 mins	2026-05-06 04:44:57.862Z	33.298° NE	2026-05-06 04:49:57.862Z	90.042° ESE	31.894°	2026-05-06 04:55:57.862Z	165.229° S
9 mins	2026-05-06 06:29:57.862Z	350.826° N	2026-05-06 06:33:57.862Z	300.082° NW	29.799°	2026-05-06 06:38:57.862Z	237.072° WSW
6 mins	2026-05-06 14:53:57.862Z	84.034° E	2026-05-06 14:55:57.862Z	61.646° ENE	17.282°	2026-05-06 14:59:57.862Z	19.671° NNE
10 mins	2026-05-06 16:34:57.862Z	171.143° S	2026-05-06 16:39:57.862Z	293.608° NW	43.672°	2026-05-06 16:44:57.862Z	340.621° 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, 28202 on other resources

View NIMBUS 2 DEB, 28202 on Heavens-Above

View NIMBUS 2 DEB, 28202 on Keep Track

View NIMBUS 2 DEB, 28202 on Celestrak

View NIMBUS 2 DEB, 28202 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, 28202

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 4 days ago

TLE from 4 days ago

TLE epoch observation values (Epoch: 2026-05-02T04:09:29.492Z)

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, 28202 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 4 days ago