NIMBUS 2 DEB, 28205

Orbit data source: Space-Track

NIMBUS 2 DEB, 28205 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/28205?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28205, 1966-040T

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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 NIMBUS 2 DEB
1 28205U 66040T   26215.61412049  .00001829  00000-0  26977-2 0  9999
2 28205 100.3332  95.5890 0044508 165.1579 224.8275 13.55245889 99101

Epoch: 2026-08-03T14:44Z

TLE epoch observation values (Epoch: 2026-08-03T14:44:20.010Z)

Latitude

29.14749°

Longitude

-83.49503°

Altitude

1,080.046 km

Speed

7.303 km/s

True Right ascension

05h 59m 07s

True Declination

29° 00' 28"

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

19:02:21

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,083.411 km

Perigee altitude

1,017.285 km

Semi-major axis

7,428.485 km

Eccentricity

0.00445

Inclination

100.3332°

RAAN

95.589°

Arg. of periapsis

165.1579°

True anomaly

224.46936°

Mean anomaly

224.8275°

Eccentric anomaly

224.64829°

Mean motion

3.38995 °/min

Orbital period

106.2 mins

BSTAR

0.0026977

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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.
12 mins	2026-08-04 05:20:41.013Z	9.956° NNE	2026-08-04 05:26:41.013Z	297.866° NW	42.658°	2026-08-04 05:32:41.013Z	208.966° SW
11 mins	2026-08-04 15:31:41.013Z	144.495° SSE	2026-08-04 15:36:41.013Z	54.191° ENE	41.268°	2026-08-04 15:42:41.013Z	351.368° N
8 mins	2026-08-04 17:17:41.013Z	226.019° WSW	2026-08-04 17:21:41.013Z	269.815° W	20.211°	2026-08-04 17:25:41.013Z	310.678° NW
10 mins	2026-08-05 04:24:41.013Z	32.657° NE	2026-08-05 04:29:41.013Z	101.634° ESE	35.131°	2026-08-05 04:34:41.013Z	168.449° 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 NIMBUS 2 DEB, 28205 on other resources

View NIMBUS 2 DEB, 28205 on Heavens-Above

View NIMBUS 2 DEB, 28205 on Keep Track

View NIMBUS 2 DEB, 28205 on Celestrak

View NIMBUS 2 DEB, 28205 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, 28205

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-08-03T14:44:20.010Z)

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, 28205 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago