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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Edit Public Description
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: 12 hours ago
TLE from 12 hours ago
0 EMISAT
1 44078U 19018A 25259.58151317 .00000192 00000-0 69704-4 0 9998
2 44078 98.5070 314.3037 0018139 325.4942 34.5069 14.43608799340584Epoch: 2025-09-16T13:57Z
TLE epoch observation values (Epoch: 2025-09-16T13:57:22.737Z)
Latitude
-0.00009°
Longitude
109.18922°
Altitude
738.909 km
Speed
7.491 km/s
True Right ascension
20h 57m 12s
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
18:16:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
756.636 km
Perigee altitude
730.799 km
Semi-major axis
7,121.854 km
Eccentricity
0.00181
Inclination
98.507°
RAAN
314.3037°
Arg. of periapsis
325.4942°
True anomaly
34.62487°
Mean anomaly
34.5069°
Eccentric anomaly
34.56586°
Mean motion
3.61122 °/min
Orbital period
99.69 mins
BSTAR
0.000069704
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-17 03:23:00.608Z | 149.985° SSE | 2025-09-17 03:27:00.608Z | 87.911° E | 40.405° | 2025-09-17 03:32:00.608Z | 354.859° N |
| 5 mins | 2025-09-17 15:32:00.608Z | 67.438° ENE | 2025-09-17 15:34:00.608Z | 97.373° ESE | 18.092° | 2025-09-17 15:37:00.608Z | 135.858° SSE |
| 8 mins | 2025-09-17 17:09:00.608Z | 355.663° N | 2025-09-17 17:13:00.608Z | 271.692° WNW | 35.559° | 2025-09-17 17:17:00.608Z | 217.441° SW |
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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