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

13.779 m², Large (>1 m²)

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

TLE from 2 days ago

0 DELTA 2 R/B
1 40060U 14035B   26282.00422477  .00000049  00000-0  00000-0 0  9992
2 40060  98.1832 113.5931 3071549  79.2343 313.4775  6.11245903273859

Epoch: 2026-10-09T00:06Z

TLE epoch observation values (Epoch: 2026-10-09T00:06:05.020Z)

Latitude

-0.00001°

Longitude

94.43268°

Altitude

4,440.66 km

Speed

6.493 km/s

True Right ascension

07h 34m 20s

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

23:28:16

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

10,135.9 km

Perigee altitude

2,374.972 km

Semi-major axis

12,633.573 km

Eccentricity

0.30715

Inclination

98.1832°

RAAN

113.5931°

Arg. of periapsis

79.2343°

True anomaly

280.85383°

Mean anomaly

313.4775°

Eccentric anomaly

297.92849°

Mean motion

1.52846 °/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.
25 mins	2026-10-11 11:04:30.252Z	129.356° SE	2026-10-11 11:19:30.252Z	62.74° ENE	42.71°	2026-10-11 11:29:30.252Z	358.805° N
20 mins	2026-10-11 14:59:30.252Z	223.693° SW	2026-10-11 15:10:30.252Z	267.003° W	23.378°	2026-10-11 15:19:30.252Z	317.572° NNW
36 mins	2026-10-11 23:30:30.252Z	34.783° NE	2026-10-11 23:42:30.252Z	97.605° ESE	36.5°	2026-10-12 00:06:30.252Z	159.681° S
29 mins	2026-10-12 03:22:30.252Z	355.562° N	2026-10-12 03:32:30.252Z	296.152° NW	39.996°	2026-10-12 03:51:30.252Z	237.223° WSW

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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: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-10-09T00:06:05.020Z)

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: 2 days ago