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)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 NIMBUS 2 DEB
1 28615U 66040AE  26007.65487459  .00007015  00000-0  55805-2 0  9999
2 28615 100.2557 144.0631 0042124 210.4176 166.1826 13.91068187583467

Epoch: 2026-01-07T15:43Z

TLE epoch observation values (Epoch: 2026-01-07T15:43:01.164Z)

Latitude

16.42493°

Longitude

158.04654°

Altitude

956.953 km

Speed

7.36 km/s

True Right ascension

09h 24m 05s

True Declination

16° 20' 04"

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

00:07:07

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

952.918 km

Perigee altitude

891.415 km

Semi-major axis

7,300.303 km

Eccentricity

0.00421

Inclination

100.2557°

RAAN

144.0631°

Arg. of periapsis

210.4176°

True anomaly

166.2973°

Mean anomaly

166.1826°

Eccentric anomaly

166.24001°

Mean motion

3.47962 °/min

Orbital period

103.46 mins

BSTAR

0.0055805

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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.
7 mins	2026-01-09 07:30:25.473Z	100.48° ESE	2026-01-09 07:33:25.473Z	66.25° ENE	20.12°	2026-01-09 07:37:25.473Z	18.792° NNE
9 mins	2026-01-09 09:11:25.473Z	182.332° SSW	2026-01-09 09:15:25.473Z	259.246° W	41.21°	2026-01-09 09:20:25.473Z	335.264° NNW
9 mins	2026-01-09 21:45:25.473Z	24.319° NE	2026-01-09 21:49:25.473Z	110.857° ESE	43.066°	2026-01-09 21:54:25.473Z	186.686° SSW
6 mins	2026-01-09 23:28:25.473Z	329.429° NNW	2026-01-09 23:30:25.473Z	305.625° NW	17.33°	2026-01-09 23:34:25.473Z	260.856° W

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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 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-01-07T15:43:01.164Z)

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 day ago