Showing default

SENTINEL 1A, 39634

Orbit data source: Space-Track

SENTINEL 1A, 39634 is a payload satellite owned by ESA (ESA) in SSO that was launched on Thu, 03 Apr 2014 UTC via a SOYUZ-ST-A 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.

Loading next visibility...
Identifier
39634, 2014-016A
Orbit
SSO
Country
Flag of ESAESA
Related business
Manufacturer
Thales Alenia
Mission
Operational Civil Radar Imaging
Bus & Motor
PRISMA, AOCS
Mass
2,157 kg wet, 2,027 kg dry
Launch date (UTC)
2014-04-03 (11 years ago)
Launch vehicle
SOYUZ-ST-A
Launch site
French Guiana (FRGUI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 4 Pan, 10.5 m
Radar Cross Section
23.487 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 SENTINEL 1A
1 39634U 14016A   25259.01333016  .00000173  00000-0  46357-4 0  9997
2 39634  98.1828 265.5268 0001352  89.4002 270.7353 14.59200295610035
Epoch: 2025-09-16T00:19Z
TLE epoch observation values (Epoch: 2025-09-16T00:19:11.725Z)
Latitude
-0.00001°
Longitude
-94.48178°
Altitude
698.73 km
Speed
7.507 km/s
True Right ascension
17h 42m 06s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
00:07:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
693.795 km
Perigee altitude
691.883 km
Semi-major axis
7,070.976 km
Eccentricity
0.00014
Inclination
98.1828°
RAAN
265.5268°
Arg. of periapsis
89.4002°
True anomaly
270.71981°
Mean anomaly
270.7353°
Eccentric anomaly
270.72755°
Mean motion
3.65026 °/min
Orbital period
98.62 mins
BSTAR
0.000046357
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|