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: 16 hours ago

TLE from 16 hours ago
0 EMISAT
1 44078U 19018A   26207.65046035  .00000255  00000-0  87833-4 0  9993
2 44078  98.4632 266.2282 0019691  98.8163 261.5258 14.43653701385757
Epoch: 2026-07-26T15:36Z
TLE epoch observation values (Epoch: 2026-07-26T15:36:39.774Z)
Latitude
-0.00002°
Longitude
87.71714°
Altitude
751.502 km
Speed
7.478 km/s
True Right ascension
17h 44m 54s
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
21:04:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
757.591 km
Perigee altitude
729.544 km
Semi-major axis
7,121.704 km
Eccentricity
0.00197
Inclination
98.4632°
RAAN
266.2282°
Arg. of periapsis
98.8163°
True anomaly
261.3027°
Mean anomaly
261.5258°
Eccentric anomaly
261.41424°
Mean motion
3.61133 °/min
Orbital period
99.69 mins
BSTAR
0.000087833
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|