DELTA 1 R/B(1), 10062

Orbit data source: Space-Track

DELTA 1 R/B(1), 10062 is space debris in LEO originally from a launch on Thu, 16 Jun 1977 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/10062?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

10062, 1977-048B

Orbit

LEO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

MDAC-HB

Mission

Spacecraft

Bus & Motor

DELTA/TR-201, Unknown motor

Mass

845 kg wet, 845 kg dry

Launch date (UTC)

1977-06-16 (49 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

Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago

0 DELTA 1 R/B(1)
1 10062U 77048B   26002.25269861  .00001445  00000-0  51110-3 0  9999
2 10062  28.4125 208.3082 0727115  78.4236 289.6970 13.38861266364760

Epoch: 2026-01-02T06:03Z

TLE epoch observation values (Epoch: 2026-01-02T06:03:53.159Z)

Latitude

0°

Longitude

15.44113°

Altitude

964.663 km

Speed

7.443 km/s

True Right ascension

13h 53m 13s

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

16:17:35

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,662.458 km

Perigee altitude

572.429 km

Semi-major axis

7,495.581 km

Eccentricity

0.07271

Inclination

28.4125°

RAAN

208.3082°

Arg. of periapsis

78.4236°

True anomaly

281.63164°

Mean anomaly

289.697°

Eccentric anomaly

285.68609°

Mean motion

3.34453 °/min

Orbital period

107.64 mins

BSTAR

0.0005111

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Other satellites on launch #48 in the year 1977 (1977-06-16 UTC)

DELTA 1 DEB, 10063 (Decayed)

DELTA 1 DEB, 10067 (Decayed)

GOES 2 AKM, 20799

GOES 2, 10061

DELTA 1 R/B(2), 10409 (Decayed)

DELTA 1 DEB, 10075 (Decayed)

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DELTA 1 R/B(1) 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	2026-01-02 18:54:46.063Z	204.685° SW	2026-01-02 18:56:46.063Z	173.295° S	15.296°	2026-01-02 18:58:46.063Z	141.624° SSE
4 mins	2026-01-02 20:48:46.063Z	207.048° SW	2026-01-02 20:49:46.063Z	190.453° SSW	15.757°	2026-01-02 20:52:46.063Z	146.886° SSE

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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 R/B(1), 10062 on other resources

View DELTA 1 R/B(1), 10062 on Heavens-Above

View DELTA 1 R/B(1), 10062 on Keep Track

View DELTA 1 R/B(1), 10062 on Celestrak

View DELTA 1 R/B(1), 10062 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 R/B(1), 10062

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-01-02T06:03:53.159Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #48 in the year 1977 (1977-06-16 UTC)

DELTA 1 R/B(1) Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 R/B(1), 10062 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago