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.
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44078 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Operational Defense Sigint
Bus & Motor
SSB-2, AOCS
Mass
436 kg wet, ~380 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
4.485 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 EMISAT
1 44078U 19018A 26048.30943979 .00000252 00000-0 87117-4 0 9993
2 44078 98.4825 107.6838 0018147 215.6249 144.3732 14.43676369362761Epoch: 2026-02-17T07:25Z
TLE epoch observation values (Epoch: 2026-02-17T07:25:35.597Z)
Latitude
0.00004°
Longitude
-151.00581°
Altitude
759.851 km
Speed
7.469 km/s
True Right ascension
07h 10m 44s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
17:23:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
756.417 km
Perigee altitude
730.57 km
Semi-major axis
7,121.631 km
Eccentricity
0.00181
Inclination
98.4825°
RAAN
107.6838°
Arg. of periapsis
215.6249°
True anomaly
144.49411°
Mean anomaly
144.3732°
Eccentric anomaly
144.43368°
Mean motion
3.61139 °/min
Orbital period
99.68 mins
BSTAR
0.000087117
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Other satellites on launch #18 in the year 2019 (2019-04-01 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.EMISAT Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-17 16:19:38.401Z | 28.044° NE | 2026-02-17 16:23:38.401Z | 99.342° ESE | 36.771° | 2026-02-17 16:27:38.401Z | 171.351° S |
| 5 mins | 2026-02-17 17:59:38.401Z | 328.051° NNW | 2026-02-17 18:01:38.401Z | 299.534° NW | 18.176° | 2026-02-17 18:04:38.401Z | 257.678° W |
| 7 mins | 2026-02-18 03:31:38.401Z | 145.342° SSE | 2026-02-18 03:34:38.401Z | 77.751° E | 40.76° | 2026-02-18 03:38:38.401Z | 357.185° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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