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: 2 days ago

TLE from 2 days ago

0 NIMBUS 2 DEB
1 28615U 66040AE  26058.87662679  .00006648  00000-0  52334-2 0  9993
2 28615 100.2465 200.5943 0031282  88.0620  63.2979 13.91878718590581

Epoch: 2026-02-27T21:02Z

TLE epoch observation values (Epoch: 2026-02-27T21:02:20.554Z)

Latitude

27.87117°

Longitude

-87.24143°

Altitude

915.184 km

Speed

7.402 km/s

True Right ascension

01h 44m 12s

True Declination

27° 43' 56"

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

06:23:20

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

942.157 km

Perigee altitude

896.502 km

Semi-major axis

7,297.466 km

Eccentricity

0.00313

Inclination

100.2465°

RAAN

200.5943°

Arg. of periapsis

88.062°

True anomaly

63.6187°

Mean anomaly

63.2979°

Eccentric anomaly

63.45824°

Mean motion

3.48165 °/min

Orbital period

103.4 mins

BSTAR

0.0052334

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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	2026-03-02 08:49:09.927Z	144.135° SSE	2026-03-02 08:54:09.927Z	56.622° ENE	39.661°	2026-03-02 08:59:09.927Z	353.715° N
7 mins	2026-03-02 10:33:09.927Z	229.043° WSW	2026-03-02 10:36:09.927Z	265.515° W	18.642°	2026-03-02 10:40:09.927Z	310.638° NW
8 mins	2026-03-02 21:23:09.927Z	47.289° ENE	2026-03-02 21:27:09.927Z	101.811° ESE	24.654°	2026-03-02 21:31:09.927Z	150.603° SSE
9 mins	2026-03-02 23:05:09.927Z	353.816° N	2026-03-02 23:09:09.927Z	287.254° WNW	33.572°	2026-03-02 23:14:09.927Z	225.043° 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, 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: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-02-27T21:02:20.554Z)

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: 2 days ago