DELTA 1 DEB, 5975

Orbit data source: Space-Track

DELTA 1 DEB, 5975 is space debris in HEO originally from a launch on Fri, 20 Mar 1970 UTC launched from the Air Force Eastern Test Range (AFETR). 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/5975?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

5975, 1970-021C

Orbit

HEO

Last TLE update

19 hours ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1970-03-20 (55 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history

TLE from 19 hours ago

0 DELTA 1 DEB
1  5975U 70021C   25128.48749697  .00008423  00000-0  25127-2 0  9994
2  5975  25.5174 106.1855 6545564 338.0310   3.4421  3.24168378359655

Epoch: 2025-05-08T11:41Z

Definitive object data (Epoch: 2025-05-08T11:41:59.738Z)

Latitude

-0.00048°

Longitude

64.13812°

Altitude

479.935 km

Speed

9.776 km/s

True Right ascension

07h 04m 46s

True Declination

0° 00' 02"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

5.49922°

Longitude

-127.95605°

Altitude

24,894.781 km

Speed

2.196 km/s

Apparent Right ascension

18h 47m 10s

Apparent Declination

-2° 10' 60"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

14:53:58

Azimuth

113.299° SE

Elevation

22.227°

Doppler factor

Orbital elements

Apogee altitude

25,536.444 km

Perigee altitude

285.092 km

Semi-major axis

19,288.905 km

Eccentricity

0.6545564

Inclination

25.5174°

RAAN

106.1855°

Arg. of periapsis

338.031°

True anomaly

21.40598°

Mean anomaly

3.4421°

Eccentric anomaly

9.87188°

Mean motion

0.81018 °/min

BSTAR

0.0025127

Orbital period

444.35 mins

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Other satellites on launch #21 in the year 1970 (1970-03-20 UTC)

NATO 2A, 4353

DELTA 1 R/B, 4354

DELTA 1 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.
86 mins	2025-05-09 06:45:05.308Z	113.32° SE	2025-05-09 06:45:05.308Z	113.32° SE	20.711°	2025-05-09 08:11:05.308Z	121.047° SE
231 mins	2025-05-09 10:53:05.308Z	277.227° WNW	2025-05-09 12:06:05.308Z	262.158° W	21.847°	2025-05-09 14:44:05.308Z	252.247° W
62 mins	2025-05-10 00:51:05.308Z	174.487° S	2025-05-10 00:59:05.308Z	125.259° SE	24.97°	2025-05-10 01:53:05.308Z	82.387° E

Authenticating...

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Check out DELTA 1 DEB, 5975 on other resources

View DELTA 1 DEB, 5975 on Heavens-Above

View DELTA 1 DEB, 5975 on Keep Track

View DELTA 1 DEB, 5975 on Celestrak

View DELTA 1 DEB, 5975 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.