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: 9 hours ago
TLE from 9 hours ago
0 EMISAT
1 44078U 19018A 26138.20342242 .00000213 00000-0 75565-4 0 9999
2 44078 98.4665 197.1643 0017483 310.8500 49.1174 14.43672155375733Epoch: 2026-05-18T04:52Z
TLE epoch observation values (Epoch: 2026-05-18T04:52:55.697Z)
Latitude
-0.00003°
Longitude
-111.96282°
Altitude
741.204 km
Speed
7.489 km/s
True Right ascension
13h 08m 39s
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
22:23:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
755.958 km
Perigee altitude
731.056 km
Semi-major axis
7,121.644 km
Eccentricity
0.00175
Inclination
98.4665°
RAAN
197.1643°
Arg. of periapsis
310.85°
True anomaly
49.26908°
Mean anomaly
49.1174°
Eccentric anomaly
49.19322°
Mean motion
3.61138 °/min
Orbital period
99.68 mins
BSTAR
0.000075565
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-18 15:29:17.768Z | 68.803° E | 2026-05-18 15:31:17.768Z | 94.36° ESE | 13.575° | 2026-05-18 15:33:17.768Z | 118.847° SE |
| 8 mins | 2026-05-18 17:06:17.768Z | 3.782° NNE | 2026-05-18 17:10:17.768Z | 269.033° W | 41.57° | 2026-05-18 17:14:17.768Z | 207.806° SW |
| 4 mins | 2026-05-19 02:41:17.768Z | 87.193° E | 2026-05-19 02:43:17.768Z | 57.505° ENE | 17.212° | 2026-05-19 02:45:17.768Z | 30.562° NE |
| 8 mins | 2026-05-19 04:17:17.768Z | 187.204° SSW | 2026-05-19 04:21:17.768Z | 269.842° W | 38.074° | 2026-05-19 04:25:17.768Z | 334.34° NNW |
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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