NIMBUS 2 DEB, 28620

Orbit data source: Space-Track

NIMBUS 2 DEB, 28620 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/28620?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28620, 1966-040AK

Orbit

SSO

Last TLE update

2 days ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-05-15 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 2 days ago

0 NIMBUS 2 DEB
1 28620U 66040AK  25180.18018771  .00001628  00000-0  25937-2 0  9998
2 28620 100.4454  69.3060 0036858 153.0034 358.1951 13.50757295  3524

Epoch: 2025-06-29T04:19Z

TLE epoch observation values (Epoch: 2025-06-29T04:19:28.218Z)

Latitude

28.33833°

Longitude

-87.3932°

Altitude

1,045.388 km

Speed

7.345 km/s

True Right ascension

16h 59m 55s

True Declination

28° 12' 02"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

-1.05433°

Longitude

-90.92655°

Altitude

1,049.382 km

Speed

7.338 km/s

Apparent Right ascension

14h 11m 12s

Apparent Declination

-29° 41' 32"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

21:26:21

Azimuth

256.304° W

Elevation

-32.167°

Doppler factor

Orbital elements

Apogee altitude

1,094.254 km

Perigee altitude

1,039.373 km

Semi-major axis

7,444.951 km

Eccentricity

0.00369

Inclination

100.4454°

RAAN

69.306°

Arg. of periapsis

153.0034°

True anomaly

Unknown

Mean anomaly

358.1951°

Eccentric anomaly

Unknown

Mean motion

3.37871 °/min

Orbital period

106.55 mins

BSTAR

0.0025937

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

NIMBUS 2 DEB Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-01 16:09:00.392Z	147.099° SSE	2025-07-01 16:14:00.392Z	50.369° ENE	42.201°	2025-07-01 16:20:00.392Z	350.138° N
7 mins	2025-07-01 17:56:00.392Z	233.199° WSW	2025-07-01 17:59:00.392Z	265.748° W	19.071°	2025-07-01 18:03:00.392Z	307.105° NW
10 mins	2025-07-02 05:05:00.392Z	33.053° NE	2025-07-02 05:09:00.392Z	87.612° E	37.058°	2025-07-02 05:15:00.392Z	174.05° S
9 mins	2025-07-02 06:50:00.392Z	347.034° N	2025-07-02 06:54:00.392Z	300.367° NW	25.02°	2025-07-02 06:59:00.392Z	244.915° WSW

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Check out NIMBUS 2 DEB, 28620 on other resources

View NIMBUS 2 DEB, 28620 on Heavens-Above

View NIMBUS 2 DEB, 28620 on Keep Track

View NIMBUS 2 DEB, 28620 on Celestrak

View NIMBUS 2 DEB, 28620 on Gunter's Space Page

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