DELTA 1 DEB, 28443

Orbit data source: Space-Track

DELTA 1 DEB, 28443 is space debris in LEO originally from a launch on Thu, 08 Feb 1962 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/28443?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28443, 1962-002E

Orbit

LEO

Last TLE update

7 hours ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

LM/EW

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1962-02-08 (63 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 7 hours ago

0 DELTA 1 DEB
1 28443U 62002E   25182.57343470  .00000298  00000-0  10119-3 0  9996
2 28443  48.2690 253.3088 0072595 219.0755 280.1387 14.58192880256163

Epoch: 2025-07-01T13:45Z

TLE epoch observation values (Epoch: 2025-07-01T13:45:44.758Z)

Latitude

29.8036°

Longitude

-83.53475°

Altitude

691.478 km

Speed

7.519 km/s

True Right ascension

02h 51m 04s

True Declination

29° 39' 15"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-22.079°

Longitude

104.48297°

Altitude

721.649 km

Speed

7.486 km/s

Apparent Right ascension

17h 38m 41s

Apparent Declination

-37° 40' 22"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

08:52:44

Azimuth

102.577° ESE

Elevation

-52.591°

Doppler factor

Orbital elements

Apogee altitude

751.428 km

Perigee altitude

648.66 km

Semi-major axis

7,078.181 km

Eccentricity

0.00726

Inclination

48.269°

RAAN

253.3088°

Arg. of periapsis

219.0755°

True anomaly

Unknown

Mean anomaly

280.1387°

Eccentric anomaly

Unknown

Mean motion

3.64469 °/min

Orbital period

98.77 mins

BSTAR

0.00010119

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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

TIROS 4, 226

DELTA 1 DEB (YO), 227

DELTA 1 DEB (YO), 228

DELTA 1 R/B, 229 (Decayed)

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.
9 mins	2025-07-02 07:22:31.036Z	216.442° SW	2025-07-02 07:27:31.036Z	137.442° SSE	38.376°	2025-07-02 07:31:31.036Z	69.574° E
8 mins	2025-07-02 09:07:31.036Z	271.671° WNW	2025-07-02 09:10:31.036Z	322.876° NNW	36.548°	2025-07-02 09:15:31.036Z	53.105° ENE
7 mins	2025-07-02 10:52:31.036Z	311.655° NW	2025-07-02 10:55:31.036Z	7.193° NNE	27.905°	2025-07-02 10:59:31.036Z	61.871° ENE
8 mins	2025-07-02 12:35:31.036Z	309.53° NW	2025-07-02 12:39:31.036Z	23.277° NE	36.91°	2025-07-02 12:43:31.036Z	92.529° ESE
8 mins	2025-07-02 14:19:31.036Z	286.955° WNW	2025-07-02 14:22:31.036Z	235.427° WSW	36.844°	2025-07-02 14:27:31.036Z	144.919° SSE

Authenticating...

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Check out DELTA 1 DEB, 28443 on other resources

View DELTA 1 DEB, 28443 on Heavens-Above

View DELTA 1 DEB, 28443 on Keep Track

View DELTA 1 DEB, 28443 on Celestrak

View DELTA 1 DEB, 28443 on Gunter's Space Page

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