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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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Identifier
40697, 2015-028A
Orbit
SSO
Country
Flag of ESAESA
Related 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)
2015-06-23 (11 years ago)
Launch vehicle
VEGA
Launch site
French Guiana (FRGUI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 6.0 m
Radar Cross Section
11.901 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 SENTINEL 2A
1 40697U 15028A   26297.30550554  .00000020  00000-0  24341-4 0  9995
2 40697  98.5638  10.2687 0001100  95.7182 264.4126 14.30824633592190
Epoch: 2026-10-24T07:19Z
TLE epoch observation values (Epoch: 2026-10-24T07:19:55.678Z)
Latitude
-0.00007°
Longitude
-132.42688°
Altitude
791.987 km
Speed
7.458 km/s
True Right ascension
00h 41m 04s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
08:42:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
786.901 km
Perigee altitude
785.325 km
Semi-major axis
7,164.25 km
Eccentricity
0.00011
Inclination
98.5638°
RAAN
10.2687°
Arg. of periapsis
95.7182°
True anomaly
264.40005°
Mean anomaly
264.4126°
Eccentric anomaly
264.40633°
Mean motion
3.57921 °/min
Orbital period
100.58 mins
BSTAR
0.000024341
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Other satellites on launch #28 in the year 2015 (2015-06-23 UTC)

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