NIMBUS 2 DEB, 28206

Orbit data source: Space-Track

NIMBUS 2 DEB, 28206 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/28206?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28206, 1966-040U

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: 8 hours ago

TLE from 8 hours ago

0 NIMBUS 2 DEB
1 28206U 66040U   26128.18245441  .00001398  00000-0  22982-2 0  9998
2 28206 100.3747  18.7072 0047370 113.2676  52.0072 13.48867571 86600

Epoch: 2026-05-08T04:22Z

TLE epoch observation values (Epoch: 2026-05-08T04:22:44.061Z)

Latitude

14.02906°

Longitude

-90.3859°

Altitude

1,056.824 km

Speed

7.335 km/s

True Right ascension

13h 25m 15s

True Declination

13° 57' 06"

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

20:17:08

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,109.066 km

Perigee altitude

1,038.467 km

Semi-major axis

7,451.903 km

Eccentricity

0.00474

Inclination

100.3747°

RAAN

18.7072°

Arg. of periapsis

113.2676°

True anomaly

52.43655°

Mean anomaly

52.0072°

Eccentric anomaly

52.22172°

Mean motion

3.37398 °/min

Orbital period

106.7 mins

BSTAR

0.0022982

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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	2026-05-08 16:09:15.029Z	145.326° SSE	2026-05-08 16:14:15.029Z	57.688° ENE	41.558°	2026-05-08 16:20:15.029Z	351.209° N
7 mins	2026-05-08 17:56:15.029Z	229.834° WSW	2026-05-08 17:59:15.029Z	262.411° W	19.722°	2026-05-08 18:03:15.029Z	305.949° NW
10 mins	2026-05-09 05:06:15.029Z	33.335° NE	2026-05-09 05:11:15.029Z	115.06° SE	36.523°	2026-05-09 05:16:15.029Z	172.779° S
8 mins	2026-05-09 06:52:15.029Z	341.263° N	2026-05-09 06:55:15.029Z	303.751° NW	25.352°	2026-05-09 07:00:15.029Z	245.525° WSW

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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, 28206 on other resources

View NIMBUS 2 DEB, 28206 on Heavens-Above

View NIMBUS 2 DEB, 28206 on Keep Track

View NIMBUS 2 DEB, 28206 on Celestrak

View NIMBUS 2 DEB, 28206 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, 28206

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-05-08T04:22:44.061Z)

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, 28206 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago