NIMBUS 2 DEB, 28615

Orbit data source: Space-Track

NIMBUS 2 DEB, 28615 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/28615?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28615, 1966-040AE

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: 1 week ago

TLE from 1 week ago

0 NIMBUS 2 DEB
1 28615U 66040AE  26149.38854196  .00007431  00000-0  57239-2 0  9997
2 28615 100.2433 300.6056 0038137 193.3190 194.9027 13.92957125603189

Epoch: 2026-05-29T09:19Z

TLE epoch observation values (Epoch: 2026-05-29T09:19:30.025Z)

Latitude

27.66492°

Longitude

-91.59669°

Altitude

948.495 km

Speed

7.366 km/s

True Right ascension

19h 40m 47s

True Declination

27° 31' 39"

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

03:04:42

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

943.376 km

Perigee altitude

887.744 km

Semi-major axis

7,293.697 km

Eccentricity

0.00381

Inclination

100.2433°

RAAN

300.6056°

Arg. of periapsis

193.319°

True anomaly

194.79082°

Mean anomaly

194.9027°

Eccentric anomaly

194.84671°

Mean motion

3.48435 °/min

Orbital period

103.32 mins

BSTAR

0.0057239

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Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)

THOR AGENA B R/B, 2174

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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	2026-06-05 22:46:36.750Z	24.755° NE	2026-06-05 22:51:36.750Z	102.268° ESE	40.661°	2026-06-05 22:56:36.750Z	180.964° SSW
6 mins	2026-06-06 00:30:36.750Z	331.117° NNW	2026-06-06 00:32:36.750Z	305.858° NW	19.154°	2026-06-06 00:36:36.750Z	257.63° W
6 mins	2026-06-06 08:42:36.750Z	93.9° ESE	2026-06-06 08:45:36.750Z	55.348° ENE	20.066°	2026-06-06 08:48:36.750Z	20.307° NNE
9 mins	2026-06-06 10:22:36.750Z	182.626° SSW	2026-06-06 10:26:36.750Z	254.777° W	40.819°	2026-06-06 10:31:36.750Z	334.744° NNW

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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, 28615 on other resources

View NIMBUS 2 DEB, 28615 on Heavens-Above

View NIMBUS 2 DEB, 28615 on Keep Track

View NIMBUS 2 DEB, 28615 on Celestrak

View NIMBUS 2 DEB, 28615 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, 28615

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 week ago

TLE from 1 week ago

TLE epoch observation values (Epoch: 2026-05-29T09:19:30.025Z)

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, 28615 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 week ago