Showing default

HYSIS, 43719

Orbit data source: Space-Track

HYSIS, 43719 is a payload satellite owned by ISRO (IN) in SSO that was launched on Thu, 29 Nov 2018 UTC via a PSLV launch vehicle from the Sirharikota (SRI). 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
43719, 2018-096A
Orbit
SSO
Country
Flag of ININ / IND
Related business
Manufacturer
ISRO
Mission
Operational Civil Imaging
Bus & Motor
SSB-2, AOCS
Mass
380 kg wet, ~350 kg dry
Launch date (UTC)
2018-11-29 (7 years ago)
Launch vehicle
PSLV
Launch site
Sirharikota (SRI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
4.485 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 HYSIS
1 43719U 18096A   26135.32379657  .00000019  00000-0  97192-5 0  9990
2 43719  97.9856 202.3262 0000882 107.8025 252.3282 14.78619577402564
Epoch: 2026-05-15T07:46Z
TLE epoch observation values (Epoch: 2026-05-15T07:46:16.023Z)
Latitude
-0.00005°
Longitude
-147.29731°
Altitude
636.89 km
Speed
7.54 km/s
True Right ascension
13h 29m 18s
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
15:38:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
631.35 km
Perigee altitude
630.113 km
Semi-major axis
7,008.868 km
Eccentricity
0.00009
Inclination
97.9856°
RAAN
202.3262°
Arg. of periapsis
107.8025°
True anomaly
252.31857°
Mean anomaly
252.3282°
Eccentric anomaly
252.32339°
Mean motion
3.69889 °/min
Orbital period
97.33 mins
BSTAR
0.0000097192
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|