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: 21 hours ago

TLE from 21 hours ago

0 DELTA 2 R/B
1 40060U 14035B   26254.51423239  .00000042  00000-0  00000-0 0  9997
2 40060  98.1864 109.2425 3069267  92.9840 302.0896  6.11246003272176

Epoch: 2026-09-11T12:20Z

TLE epoch observation values (Epoch: 2026-09-11T12:20:29.678Z)

Latitude

-0°

Longitude

-66.42431°

Altitude

5,248.534 km

Speed

6.085 km/s

True Right ascension

07h 16m 56s

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

01:28:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

10,133.016 km

Perigee altitude

2,377.855 km

Semi-major axis

12,633.572 km

Eccentricity

0.30693

Inclination

98.1864°

RAAN

109.2425°

Arg. of periapsis

92.984°

True anomaly

267.1204°

Mean anomaly

302.0896°

Eccentric anomaly

285.11215°

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.
24 mins	2026-09-12 12:02:27.109Z	113.555° SE	2026-09-12 12:16:27.109Z	61.132° ENE	32.178°	2026-09-12 12:26:27.109Z	3.219° NNE
32 mins	2026-09-12 15:46:27.109Z	197.689° SSW	2026-09-12 16:07:27.109Z	266.207° W	39.953°	2026-09-12 16:18:27.109Z	330.087° NNW
22 mins	2026-09-13 00:29:27.109Z	47.928° ENE	2026-09-13 00:38:27.109Z	92.682° ESE	20.659°	2026-09-13 00:51:27.109Z	134.713° SE
28 mins	2026-09-13 04:19:27.109Z	0.916° NNE	2026-09-13 04:29:27.109Z	290.75° WNW	51.971°	2026-09-13 04:47:27.109Z	223.209° SW

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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: 21 hours ago

TLE from 21 hours ago

TLE epoch observation values (Epoch: 2026-09-11T12:20:29.678Z)

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: 21 hours ago