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)

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   26171.22028235  .00000015  00000-0  00000+0 0  9999
2 40060  98.2027  96.0416 3069582 134.7025 254.8972  6.11243056267089

Epoch: 2026-06-20T05:17Z

TLE epoch observation values (Epoch: 2026-06-20T05:17:12.395Z)

Latitude

0.00005°

Longitude

108.30406°

Altitude

8,215.743 km

Speed

4.805 km/s

True Right ascension

06h 24m 10s

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

21:42:37

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

10,133.467 km

Perigee altitude

2,377.485 km

Semi-major axis

12,633.613 km

Eccentricity

0.30696

Inclination

98.2027°

RAAN

96.0416°

Arg. of periapsis

134.7025°

True anomaly

225.36758°

Mean anomaly

254.8972°

Eccentric anomaly

239.71066°

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.
44 mins	2026-06-22 16:17:34.831Z	117.257° SE	2026-06-22 16:46:34.831Z	58.304° ENE	33.784°	2026-06-22 17:01:34.831Z	356.95° N
60 mins	2026-06-22 19:53:34.831Z	186.771° SSW	2026-06-22 20:33:34.831Z	258.876° W	37.764°	2026-06-22 20:53:34.831Z	337.86° N
10 mins	2026-06-23 05:04:34.831Z	53.44° ENE	2026-06-23 05:09:34.831Z	82.616° E	14.466°	2026-06-23 05:14:34.831Z	109.969° ESE
21 mins	2026-06-23 08:52:34.831Z	2.784° NNE	2026-06-23 09:02:34.831Z	296.74° NW	35.659°	2026-06-23 09:13:34.831Z	228.114° 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: 2026-06-20T05:17:12.395Z)

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