SENTINEL 2A, 40697
Orbit data source: Space-Track
SENTINEL 2A, 40697 is an ESA payload satellite in SSO that was launched on Tue, 23 Jun 2015 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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40697 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: 9 hours ago
TLE from 9 hours ago
0 SENTINEL 2A
1 40697U 15028A 26285.27757977 .00000023 00000-0 25223-4 0 9999
2 40697 98.5651 358.4211 0001054 92.4878 267.6425 14.30821153590479Epoch: 2026-10-12T06:39Z
TLE epoch observation values (Epoch: 2026-10-12T06:39:42.892Z)
Latitude
-0.00006°
Longitude
-122.36592°
Altitude
791.952 km
Speed
7.458 km/s
True Right ascension
23h 53m 41s
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
10:27:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
786.88 km
Perigee altitude
785.369 km
Semi-major axis
7,164.262 km
Eccentricity
0.00011
Inclination
98.5651°
RAAN
358.4211°
Arg. of periapsis
92.4878°
True anomaly
267.63043°
Mean anomaly
267.6425°
Eccentric anomaly
267.63647°
Mean motion
3.5792 °/min
Orbital period
100.58 mins
BSTAR
0.000025223
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Other satellites on launch #28 in the year 2015 (2015-06-23 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 2A 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-10-12 17:18:27.325Z | 28.503° NE | 2026-10-12 17:23:27.325Z | 102.853° ESE | 40.702° | 2026-10-12 17:27:27.325Z | 164.864° S |
| 7 mins | 2026-10-12 18:59:27.325Z | 338.374° N | 2026-10-12 19:02:27.325Z | 295.457° NW | 24.206° | 2026-10-12 19:06:27.325Z | 243.197° WSW |
| 9 mins | 2026-10-13 04:36:27.325Z | 146.308° SSE | 2026-10-13 04:40:27.325Z | 68.435° E | 56.911° | 2026-10-13 04:45:27.325Z | 355.259° N |
| 4 mins | 2026-10-13 06:18:27.325Z | 245.246° WSW | 2026-10-13 06:20:27.325Z | 272.126° WNW | 16.513° | 2026-10-13 06:22:27.325Z | 297.585° NW |
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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