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SENTINEL 3A, 41335

Orbit data source: Space-Track

SENTINEL 3A, 41335 is an ESA payload satellite in SSO that was launched on Tue, 16 Feb 2016 UTC via an ROKOT launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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
41335, 2016-011A
Orbit
SSO
Last TLE update
9 hours ago
Origin
Manufacturer
Thales Alenia
Mission
Operational Civil Imaging
Bus & Motor
SENTINEL-3A, Unknown motor
Mass
1,250 kg wet, 1,150 kg dry
Launch date (UTC)
2016-02-16 (9 years ago)
Launch vehicle
ROKOT
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 6.9 m
Radar Cross Section
12.454 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago
0 SENTINEL 3A
1 41335U 16011A   25128.91776626  .00000167  00000-0  87240-4 0  9996
2 41335  98.6267 197.0658 0000995 105.6166 254.5125 14.26737379480410
Epoch: 2025-05-08T22:01Z
Definitive object data (Epoch: 2025-05-08T22:01:35.004Z)
Latitude
0.00002°
Longitude
-0.31143°
Altitude
805.774 km
Speed
7.45 km/s
True Right ascension
13h 08m 15s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization TLE readout
Latitude
72.17915°
Longitude
-151.94782°
Altitude
814.346 km
Speed
7.453 km/s
Apparent Right ascension
03h 04m 01s
Apparent Declination
21° 11' 13"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
15:05:03
Azimuth
0.276° NNE
Elevation
-28.896°
Doppler factor
1
Orbital elements
Apogee altitude
800.517 km
Perigee altitude
799.089 km
Semi-major axis
7,177.94 km
Eccentricity
0.0000995
Inclination
98.6267°
RAAN
197.0658°
Arg. of periapsis
105.6166°
True anomaly
254.50151°
Mean anomaly
254.5125°
Eccentric anomaly
254.50701°
Mean motion
3.56897 °/min
BSTAR
0.00008724
Orbital period
100.87 mins
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Other satellites on launch #11 in the year 2016 (2016-02-16 UTC)

SENTINEL 3A Visibility forecast

Observer location: undefined°, undefined°

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 mins2025-05-09 17:07:08.575Z21.942° NNE2025-05-09 17:12:08.575Z123.282° SE40.765°2025-05-09 17:16:08.575Z180.054° SSW
5 mins2025-05-09 18:49:08.575Z322.116° NNW2025-05-09 18:51:08.575Z295.339° NW16.43°2025-05-09 18:54:08.575Z259.517° W
8 mins2025-05-10 04:27:08.575Z164.205° S2025-05-10 04:31:08.575Z352.281° N44.041°2025-05-10 04:35:08.575Z347.042° N
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