Showing default

SENTINEL-2C, 60989

Orbit data source: Space-Track

SENTINEL-2C, 60989 is an ESA payload satellite in SSO that was launched on Thu, 05 Sep 2024 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.

Loading next visibility...
Identifier
60989, 2024-157A
Orbit
SSO
Country
Flag of ESAESA
Related business
Manufacturer
ADS/Bremen
Mission
Operational Civil Imaging
Bus & Motor
SENTINEL-2, AOCS
Mass
1,143 kg wet, 1,010 kg dry
Launch date (UTC)
2024-09-05 (2 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: 9 hours ago

TLE from 9 hours ago
0 SENTINEL-2C
1 60989U 24157A   26171.45925764  .00000070  00000-0  43396-4 0  9996
2 60989  98.5692 246.1950 0000995  83.4152 276.7144 14.30818579 93454
Epoch: 2026-06-20T11:01Z
TLE epoch observation values (Epoch: 2026-06-20T11:01:19.860Z)
Latitude
-0.00001°
Longitude
172.18867°
Altitude
791.846 km
Speed
7.458 km/s
True Right ascension
16h 24m 46s
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
07:15:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
786.846 km
Perigee altitude
785.421 km
Semi-major axis
7,164.27 km
Eccentricity
0.0001
Inclination
98.5692°
RAAN
246.195°
Arg. of periapsis
83.4152°
True anomaly
276.70308°
Mean anomaly
276.7144°
Eccentric anomaly
276.70874°
Mean motion
3.57919 °/min
Orbital period
100.58 mins
BSTAR
0.000043396
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...
Other satellites on launch #157 in the year 2024 (2024-09-05 UTC)

Documentation

Showing up to 5 results
|