WORLDVIEW 2, 35946
Orbit data source: Space-Track
WORLDVIEW 2, 35946 is a payload satellite owned by DigitalGlobe (US) in SSO that was launched on Thu, 08 Oct 2009 UTC via a DELTA 7920-10C 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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35946 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: 8 hours ago
TLE from 8 hours ago
0 WORLDVIEW 2
1 35946U 09055A 26295.92241467 .00000112 00000-0 51534-4 0 9991
2 35946 98.4738 7.6073 0004168 185.9079 174.2059 14.37929529894009Epoch: 2026-10-22T22:08Z
TLE epoch observation values (Epoch: 2026-10-22T22:08:16.627Z)
Latitude
-0.00009°
Longitude
4.18767°
Altitude
771.257 km
Speed
7.467 km/s
True Right ascension
00h 30m 25s
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
01:02:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
765.447 km
Perigee altitude
759.495 km
Semi-major axis
7,140.608 km
Eccentricity
0.00042
Inclination
98.4738°
RAAN
7.6073°
Arg. of periapsis
185.9079°
True anomaly
174.21072°
Mean anomaly
174.2059°
Eccentric anomaly
174.20831°
Mean motion
3.597 °/min
Orbital period
100.08 mins
BSTAR
0.000051534
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Other satellites on launch #55 in the year 2009 (2009-10-08 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 2 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-10-23 17:05:27.082Z | 34.007° NE | 2026-10-23 17:09:27.082Z | 89.074° E | 33.157° | 2026-10-23 17:13:27.082Z | 155.84° SSE |
| 7 mins | 2026-10-23 18:45:27.082Z | 341.877° N | 2026-10-23 18:48:27.082Z | 296.423° NW | 27.657° | 2026-10-23 18:52:27.082Z | 238.605° WSW |
| 7 mins | 2026-10-24 04:20:27.082Z | 132.261° SE | 2026-10-24 04:23:27.082Z | 76.642° E | 43.12° | 2026-10-24 04:27:27.082Z | 4.905° NNE |
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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