Showing default

EMISAT, 44078

Orbit data source: Space-Track

EMISAT, 44078 is a payload satellite owned by ISRO (IN) in SSO that was launched on Mon, 01 Apr 2019 UTC via a PSLV-QL 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
44078, 2019-018A
Orbit
SSO
Country
Flag of ININ / IND
Related business
Manufacturer
ISRO
Mission
Operational Defense Sigint
Bus & Motor
SSB-2, AOCS
Mass
436 kg wet, ~380 kg dry
Launch date (UTC)
2019-04-01 (7 years ago)
Launch vehicle
PSLV-QL
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: 8 hours ago

TLE from 8 hours ago
0 EMISAT
1 44078U 19018A   26015.18006926  .00000004  00000-0  14389-4 0  9991
2 44078  98.4891  74.6625 0018061 321.1931  38.7961 14.43651060357986
Epoch: 2026-01-15T04:19Z
TLE epoch observation values (Epoch: 2026-01-15T04:19:17.984Z)
Latitude
-0.00001°
Longitude
-104.79984°
Altitude
739.393 km
Speed
7.49 km/s
True Right ascension
04h 58m 39s
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
12:48:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
756.44 km
Perigee altitude
730.715 km
Semi-major axis
7,121.714 km
Eccentricity
0.00181
Inclination
98.4891°
RAAN
74.6625°
Arg. of periapsis
321.1931°
True anomaly
38.926°
Mean anomaly
38.7961°
Eccentric anomaly
38.86103°
Mean motion
3.61132 °/min
Orbital period
99.69 mins
BSTAR
0.000014389
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|