SENTINEL 2B, 42063
Orbit data source: Space-Track
SENTINEL 2B, 42063 is an ESA payload satellite in SSO that was launched on Tue, 07 Mar 2017 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). 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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42063 intel report (Beta)
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Identifier
Orbit
Country
ESARelated business
Manufacturer
ADS/Bremen
Mission
Operational Civil Imaging
Bus & Motor
SENTINEL-2, AOCS
Mass
1,130 kg wet, 1,063 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 6.0 m
Radar Cross Section
11.901 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 SENTINEL 2B
1 42063U 17013A 26172.47322568 .00000345 00000-0 14824-3 0 9996
2 42063 98.5686 247.1877 0001181 88.2642 271.8676 14.30818862485258Epoch: 2026-06-21T11:21Z
TLE epoch observation values (Epoch: 2026-06-21T11:21:26.698Z)
Latitude
-0.00006°
Longitude
167.15347°
Altitude
791.901 km
Speed
7.458 km/s
True Right ascension
16h 28m 45s
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
21:31:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
786.979 km
Perigee altitude
785.286 km
Semi-major axis
7,164.269 km
Eccentricity
0.00012
Inclination
98.5686°
RAAN
247.1877°
Arg. of periapsis
88.2642°
True anomaly
271.85407°
Mean anomaly
271.8676°
Eccentric anomaly
271.86084°
Mean motion
3.57919 °/min
Orbital period
100.58 mins
BSTAR
0.00014824
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Other satellites on launch #13 in the year 2017 (2017-03-07 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.SENTINEL 2B 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-22 16:30:26.976Z | 61.499° ENE | 2026-06-22 16:32:26.976Z | 84.543° E | 13.098° | 2026-06-22 16:34:26.976Z | 109.355° ESE |
| 8 mins | 2026-06-22 18:09:26.976Z | 4.309° NNE | 2026-06-22 18:12:26.976Z | 315.249° NNW | 42.247° | 2026-06-22 18:17:26.976Z | 205.278° SW |
| 6 mins | 2026-06-23 03:48:26.976Z | 97.723° ESE | 2026-06-23 03:50:26.976Z | 69.844° E | 19.289° | 2026-06-23 03:54:26.976Z | 18.264° NNE |
| 8 mins | 2026-06-23 05:26:26.976Z | 192.76° SSW | 2026-06-23 05:29:26.976Z | 243.599° WSW | 36.285° | 2026-06-23 05:34:26.976Z | 333.465° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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