NIMBUS 2 DEB, 28203

Orbit data source: Space-Track

NIMBUS 2 DEB, 28203 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/28203?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28203, 1966-040R

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 28203U 66040R   26211.67612260  .00000987  00000-0  15892-2 0  9994
2 28203 100.3295 102.7107 0044820 175.8407 245.0731 13.51089493190729

Epoch: 2026-07-30T16:13Z

TLE epoch observation values (Epoch: 2026-07-30T16:13:36.992Z)

Latitude

58.94599°

Longitude

-106.53264°

Altitude

1,092.313 km

Speed

7.305 km/s

True Right ascension

05h 40m 44s

True Declination

58° 48' 02"

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

16:52:39

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,098.949 km

Perigee altitude

1,032.223 km

Semi-major axis

7,443.723 km

Eccentricity

0.00448

Inclination

100.3295°

RAAN

102.7107°

Arg. of periapsis

175.8407°

True anomaly

244.60845°

Mean anomaly

245.0731°

Eccentric anomaly

244.84066°

Mean motion

3.37954 °/min

Orbital period

106.52 mins

BSTAR

0.0015892

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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	2026-08-04 04:57:20.244Z	37.474° NE	2026-08-04 05:02:20.244Z	101.598° ESE	30.62°	2026-08-04 05:07:20.244Z	161.137° S
9 mins	2026-08-04 06:43:20.244Z	348.774° N	2026-08-04 06:47:20.244Z	290.667° WNW	30.846°	2026-08-04 06:52:20.244Z	233.209° WSW
7 mins	2026-08-04 15:11:20.244Z	90.922° ESE	2026-08-04 15:14:20.244Z	57.808° ENE	19.738°	2026-08-04 15:18:20.244Z	16.982° NNE
11 mins	2026-08-04 16:53:20.244Z	173.231° S	2026-08-04 16:58:20.244Z	236.175° WSW	43.357°	2026-08-04 17:04:20.244Z	339.003° 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, 28203 on other resources

View NIMBUS 2 DEB, 28203 on Heavens-Above

View NIMBUS 2 DEB, 28203 on Keep Track

View NIMBUS 2 DEB, 28203 on Celestrak

View NIMBUS 2 DEB, 28203 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, 28203

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: 2026-07-30T16:13:36.992Z)

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, 28203 on other resources

Documentation

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