DELTA 1 DEB (YO), 228

Orbit data source: Space-Track

DELTA 1 DEB (YO), 228 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/228?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

228, 1962-002C

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)

1962-02-08 (64 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

Medium (>0.1 m² and <1 m²)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 DELTA 1 DEB (YO)
1 00228U 62002C   26177.63358486  .00029347  00000-0  45897-3 0  9999
2 00228  48.4296 267.2157 0004238 244.2339 115.8169 15.53415792444578

Epoch: 2026-06-26T15:12Z

TLE epoch observation values (Epoch: 2026-06-26T15:12:21.731Z)

Latitude

-0.00002°

Longitude

124.36585°

Altitude

408.4 km

Speed

7.667 km/s

True Right ascension

17h 48m 51s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

02:15:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

410.683 km

Perigee altitude

404.931 km

Semi-major axis

6,785.944 km

Eccentricity

0.00042

Inclination

48.4296°

RAAN

267.2157°

Arg. of periapsis

244.2339°

True anomaly

115.86061°

Mean anomaly

115.8169°

Eccentric anomaly

115.83875°

Mean motion

3.88265 °/min

Orbital period

92.72 mins

BSTAR

0.00045897

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

DELTA 1 DEB (YO), 227

DELTA 1 DEB, 28443

DELTA 1 R/B, 229 (Decayed)

TIROS 4, 226

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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.
4 mins	2026-06-28 09:06:57.646Z	249.743° W	2026-06-28 09:08:57.646Z	18.623° NNE	42.11°	2026-06-28 09:10:57.646Z	53.587° ENE
4 mins	2026-06-28 13:58:57.646Z	318.351° NNW	2026-06-28 14:00:57.646Z	46.616° ENE	37.602°	2026-06-28 14:02:57.646Z	99.759° ESE

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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), 228 on other resources

View DELTA 1 DEB (YO), 228 on Heavens-Above

View DELTA 1 DEB (YO), 228 on Keep Track

View DELTA 1 DEB (YO), 228 on Celestrak

View DELTA 1 DEB (YO), 228 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), 228

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-06-26T15:12:21.731Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

DELTA 1 DEB (YO) Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 DEB (YO), 228 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago