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SENTINEL 1C, 62261

Orbit data source: Space-Track

SENTINEL 1C, 62261 is an ESA payload satellite in SSO that was launched on Thu, 05 Dec 2024 UTC via a VEGA C 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
62261, 2024-235A
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)
2024-12-05 (9 months ago)
Launch vehicle
VEGA C
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: 20 hours ago

TLE from 20 hours ago
0 SENTINEL 1C
1 62261U 24235A   25239.98402127  .00000018  00000-0  13578-4 0  9994
2 62261  98.1823 246.5049 0001356  89.8297 270.3058 14.59198854 38659
Epoch: 2025-08-27T23:36Z
TLE epoch observation values (Epoch: 2025-08-27T23:36:59.437Z)
Latitude
-0.00005°
Longitude
-84.19629°
Altitude
698.742 km
Speed
7.507 km/s
True Right ascension
16h 26m 01s
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
10:59:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
693.802 km
Perigee altitude
691.885 km
Semi-major axis
7,070.98 km
Eccentricity
0.00014
Inclination
98.1823°
RAAN
246.5049°
Arg. of periapsis
89.8297°
True anomaly
270.29026°
Mean anomaly
270.3058°
Eccentric anomaly
270.29803°
Mean motion
3.65026 °/min
Orbital period
98.62 mins
BSTAR
0.000013578
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Other satellites on launch #235 in the year 2024 (2024-12-05 UTC)

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