DELTA 1 DEB, 2154

Orbit data source: Space-Track

DELTA 1 DEB, 2154 is space debris in SSO originally from a launch on Thu, 03 Feb 1966 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/2154?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2154, 1966-008E

Orbit

SSO

Last TLE update

1 day ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-02-03 (59 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

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 DELTA 1 DEB
1 02154U 66008E   25181.28074131  .00000647  00000-0  11267-3 0  9992
2 02154  97.8400 304.7651 0046992 357.0396   3.0526 14.70611786127277

Epoch: 2025-06-30T06:44Z

TLE epoch observation values (Epoch: 2025-06-30T06:44:16.049Z)

Latitude

0.00001°

Longitude

-74.89458°

Altitude

629.097 km

Speed

7.562 km/s

True Right ascension

20h 19m 03s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

-73.27978°

Longitude

79.01031°

Altitude

690.805 km

Speed

7.507 km/s

Apparent Right ascension

07h 36m 12s

Apparent Declination

-57° 42' 58"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

20:01:34

Azimuth

169.151° S

Elevation

-71.736°

Doppler factor

Orbital elements

Apogee altitude

689.222 km

Perigee altitude

623.111 km

Semi-major axis

7,034.303 km

Eccentricity

0.0047

Inclination

97.84°

RAAN

304.7651°

Arg. of periapsis

357.0396°

True anomaly

Unknown

Mean anomaly

3.0526°

Eccentric anomaly

Unknown

Mean motion

3.67885 °/min

Orbital period

97.86 mins

BSTAR

0.00011267

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Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

ESSA 1 (OT-3), 1982

DELTA 1 R/B, 1983

DELTA 1 DEB, 2085 (Decayed)

DELTA 1 DEB, 2118

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.
6 mins	2025-07-01 08:59:27.900Z	210.402° SW	2025-07-01 09:02:27.900Z	265.902° W	25.83°	2025-07-01 09:05:27.900Z	318.658° NNW
7 mins	2025-07-01 20:52:27.900Z	23.401° NE	2025-07-01 20:55:27.900Z	76.764° E	40.751°	2025-07-01 20:59:27.900Z	179.025° S
6 mins	2025-07-02 07:52:27.900Z	135.524° SSE	2025-07-02 07:54:27.900Z	87.175° E	36.421°	2025-07-02 07:58:27.900Z	1.236° NNE

Authenticating...

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Check out DELTA 1 DEB, 2154 on other resources

View DELTA 1 DEB, 2154 on Heavens-Above

View DELTA 1 DEB, 2154 on Keep Track

View DELTA 1 DEB, 2154 on Celestrak

View DELTA 1 DEB, 2154 on Gunter's Space Page

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