WORLDVIEW 3, 40115
Orbit data source: Space-Track
WORLDVIEW 3, 40115 is a payload satellite owned by DigitalGlobe (US) in SSO that was launched on Wed, 13 Aug 2014 UTC via an ATLAS V 401 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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40115 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Ball
Mission
Operational Commercial Imaging
Bus & Motor
BCP-5000, Unknown motor
Mass
2,615 kg wet, ~2,200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 2 Pan, 4.4 m
Radar Cross Section
13.188 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 WORLDVIEW 3
1 40115U 14048A 26061.76705237 .00001220 00000-0 15003-3 0 9997
2 40115 97.8647 138.0513 0000666 16.0558 344.0677 14.84815513626115Epoch: 2026-03-02T18:24Z
TLE epoch observation values (Epoch: 2026-03-02T18:24:33.324Z)
Latitude
-0.00011°
Longitude
61.35672°
Altitude
616.746 km
Speed
7.551 km/s
True Right ascension
09h 12m 12s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
06:57:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
611.663 km
Perigee altitude
610.732 km
Semi-major axis
6,989.335 km
Eccentricity
0.00007
Inclination
97.8647°
RAAN
138.0513°
Arg. of periapsis
16.0558°
True anomaly
344.0656°
Mean anomaly
344.0677°
Eccentric anomaly
344.06665°
Mean motion
3.71441 °/min
Orbital period
96.92 mins
BSTAR
0.00015003
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Other satellites on launch #48 in the year 2014 (2014-08-13 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.WORLDVIEW 3 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-03 04:14:49.012Z | 126.822° SE | 2026-03-03 04:18:49.012Z | 57.362° ENE | 24.3° | 2026-03-03 04:21:49.012Z | 12.383° NNE |
| 4 mins | 2026-03-03 05:52:49.012Z | 234.838° WSW | 2026-03-03 05:53:49.012Z | 254.573° W | 21.72° | 2026-03-03 05:56:49.012Z | 310.183° NW |
| 7 mins | 2026-03-03 17:37:49.012Z | 24.655° NE | 2026-03-03 17:40:49.012Z | 94.451° ESE | 40.408° | 2026-03-03 17:44:49.012Z | 179.706° S |
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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