DELTA 1 DEB (YO), 312

Orbit data source: Space-Track

DELTA 1 DEB (YO), 312 is space debris in LEO originally from a launch on Tue, 19 Jun 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 src="https://www.satcat.com/sats-embedded/312?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/312?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

312, 1962-025C

Orbit

LEO

Last TLE update

22 hours ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

RCA/East Windsor

Mission

Spacecraft

Bus & Motor

Unknown

Mass

~1 kg wet, ~1 kg dry

Launch date (UTC)

1962-06-19 (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 22 hours ago

0 DELTA 1 DEB (YO)
1 00312U 62025C   25128.30970066  .00001849  00000-0  32043-3 0  9997
2 00312  58.2461  68.0117 0198598 123.1763 238.8490 14.60501637299748

Epoch: 2025-05-08T07:25Z

Definitive object data (Epoch: 2025-05-08T07:25:58.137Z)

Latitude

-0.00003°

Longitude

90.13741°

Altitude

767.586 km

Speed

7.432 km/s

True Right ascension

04h 32m 02s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

57.21594°

Longitude

159.70715°

Altitude

596.52 km

Speed

7.623 km/s

Apparent Right ascension

04h 25m 53s

Apparent Declination

21° 10' 30"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

13:18:00

Azimuth

315.155° NNW

Elevation

-14.848°

Doppler factor

Orbital elements

Apogee altitude

831.424 km

Perigee altitude

550.64 km

Semi-major axis

7,069.169 km

Eccentricity

0.0198598

Inclination

58.2461°

RAAN

68.0117°

Arg. of periapsis

123.1763°

True anomaly

236.92645°

Mean anomaly

238.849°

Eccentric anomaly

237.88523°

Mean motion

3.65166 °/min

BSTAR

0.00032043

Orbital period

98.59 mins

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Other satellites on launch #25 in the year 1962 (1962-06-19 UTC)

TIROS 5, 309

DELTA 1 R/B, 311 (Decayed)

DELTA 1 DEB (YO), 313 (Decayed)

DELTA 1 DEB, 6251 (Decayed)

DELTA 1 DEB (YO) 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.
7 mins	2025-05-09 05:17:23.375Z	333.604° NNW	2025-05-09 05:21:23.375Z	52.981° ENE	30.161°	2025-05-09 05:24:23.375Z	106.514° ESE
4 mins	2025-05-09 07:01:23.375Z	271.901° WNW	2025-05-09 07:03:23.375Z	228.407° WSW	21.912°	2025-05-09 07:05:23.375Z	192.783° SSW
7 mins	2025-05-09 21:22:23.375Z	188.273° SSW	2025-05-09 21:25:23.375Z	124.835° SE	34.802°	2025-05-09 21:29:23.375Z	55.821° ENE
6 mins	2025-05-09 23:05:23.375Z	278.388° WNW	2025-05-09 23:07:23.375Z	315.982° NNW	25.398°	2025-05-09 23:11:23.375Z	21.751° NNE
4 mins	2025-05-10 04:17:23.375Z	359.747° N	2025-05-10 04:19:23.375Z	35.339° NE	17.605°	2025-05-10 04:21:23.375Z	69.388° E

Authenticating...

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Check out DELTA 1 DEB (YO), 312 on other resources

View DELTA 1 DEB (YO), 312 on Heavens-Above

View DELTA 1 DEB (YO), 312 on Keep Track

View DELTA 1 DEB (YO), 312 on Celestrak

View DELTA 1 DEB (YO), 312 on Gunter's Space Page

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