DELTA 2 R/B, 40060

Orbit data source: Space-Track

DELTA 2 R/B, 40060 is space debris in HEO originally from a launch on Wed, 02 Jul 2014 UTC launched from the Air Force Western Test Range (AFWTR). 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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https://www.satcat.com/sats-embedded/40060?theme=dark&initialShowStats=false

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Identifier

40060, 2014-035B

Orbit

HEO

Country

Related business

Boeing (US)

Manufacturer

Boeing/Pueblo

Mission

Spacecraft

Bus & Motor

DELTA/0020, Unknown motor

Mass

~924 kg wet, 924 kg dry

Launch date (UTC)

2014-07-02 (12 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + Cone, 3.0 m

Radar Cross Section

13.836 m², Large (>1 m²)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 DELTA 2 R/B
1 40060U 14035B   26070.40366868  .00000038  00000-0  00000-0 0  9990
2 40060  98.2094  80.0528 3081068 185.0867 170.9715  6.11240613260921

Epoch: 2026-03-11T09:41Z

TLE epoch observation values (Epoch: 2026-03-11T09:41:16.973Z)

Latitude

0.00003°

Longitude

125.66041°

Altitude

10,124.54 km

Speed

4.095 km/s

True Right ascension

05h 20m 11s

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

17:02:46

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

10,148.02 km

Perigee altitude

2,362.996 km

Semi-major axis

12,633.645 km

Eccentricity

0.30811

Inclination

98.2094°

RAAN

80.0528°

Arg. of periapsis

185.0867°

True anomaly

174.97466°

Mean anomaly

170.9715°

Eccentric anomaly

173.09411°

Mean motion

1.52845 °/min

Orbital period

235.53 mins

BSTAR

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Other satellites on launch #35 in the year 2014 (2014-07-02 UTC)

OCO 2, 40059

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DELTA 2 R/B 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.
31 mins	2026-03-12 14:35:32.308Z	10.093° NNE	2026-03-12 14:55:32.308Z	304.749° NW	36.223°	2026-03-12 15:06:32.308Z	237.066° WSW
24 mins	2026-03-12 18:16:32.308Z	30.074° NE	2026-03-12 18:29:32.308Z	5.113° NNE	15.951°	2026-03-12 18:40:32.308Z	334.726° NNW
72 mins	2026-03-12 21:15:32.308Z	105.367° ESE	2026-03-12 22:00:32.308Z	48.159° ENE	35.446°	2026-03-12 22:27:32.308Z	349.764° N
98 mins	2026-03-13 00:40:32.308Z	171.952° S	2026-03-13 01:38:32.308Z	254.604° W	42.785°	2026-03-13 02:18:32.308Z	346.816° N
18 mins	2026-03-13 10:24:32.308Z	29.149° NE	2026-03-13 10:34:32.308Z	65.676° ENE	17.199°	2026-03-13 10:42:32.308Z	105.567° 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 2 R/B, 40060 on other resources

View DELTA 2 R/B, 40060 on Heavens-Above

View DELTA 2 R/B, 40060 on Keep Track

View DELTA 2 R/B, 40060 on Celestrak

View DELTA 2 R/B, 40060 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 2 R/B, 40060

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: 2026-03-11T09:41:16.973Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #35 in the year 2014 (2014-07-02 UTC)

DELTA 2 R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 2 R/B, 40060 on other resources

Documentation

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