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 URL

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

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ISO8601 Format

Identifier

312, 1962-025C

Orbit

LEO

Country

Related business

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 shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago

0 DELTA 1 DEB (YO)
1 00312U 62025C   25310.49549842  .00001408  00000-0  25187-3 0  9996
2 00312  58.2445 121.0626 0192951   9.7338 350.7346 14.61162077326364

Epoch: 2025-11-06T11:53Z

TLE epoch observation values (Epoch: 2025-11-06T11:53:31.063Z)

Latitude

-0.00007°

Longitude

-103.26986°

Altitude

556.286 km

Speed

7.656 km/s

True Right ascension

08h 04m 15s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

09:42:14

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

825.261 km

Perigee altitude

552.542 km

Semi-major axis

7,067.039 km

Eccentricity

0.0193

Inclination

58.2445°

RAAN

121.0626°

Arg. of periapsis

9.7338°

True anomaly

350.36993°

Mean anomaly

350.7346°

Eccentric anomaly

350.55315°

Mean motion

3.65331 °/min

Orbital period

98.54 mins

BSTAR

0.00025187

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

DELTA 1 DEB, 6251 (Decayed)

TIROS 5, 309

DELTA 1 DEB (YO), 313 (Decayed)

DELTA 1 R/B, 311 (Decayed)

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DELTA 1 DEB (YO) Visibility forecast

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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.
5 mins	2025-11-08 15:02:45.182Z	298.457° NW	2025-11-08 15:04:45.182Z	331.071° NNW	17.07°	2025-11-08 15:07:45.182Z	13.798° NNE
7 mins	2025-11-08 20:13:45.182Z	345.986° N	2025-11-08 20:16:45.182Z	47.356° ENE	30.973°	2025-11-08 20:20:45.182Z	104.369° ESE
7 mins	2025-11-08 21:55:45.182Z	291.921° WNW	2025-11-08 21:58:45.182Z	234.132° WSW	32.343°	2025-11-08 22:02:45.182Z	172.9° S
6 mins	2025-11-09 12:17:45.182Z	173.111° S	2025-11-09 12:19:45.182Z	133.169° SE	26.411°	2025-11-09 12:23:45.182Z	61.899° ENE

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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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

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

DELTA 1 DEB (YO), 312

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2025-11-06T11:53:31.063Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

DELTA 1 DEB (YO) Visibility forecast

Co-orbital & Co-planar RSOs

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

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago