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: 9 hours ago
TLE from 9 hours ago
0 EMISAT
1 44078U 19018A 25298.94965529 .00000358 00000-0 11834-3 0 9993
2 44078 98.5002 353.6225 0018603 200.6335 159.4106 14.43646613346267Epoch: 2025-10-25T22:47Z
TLE epoch observation values (Epoch: 2025-10-25T22:47:30.217Z)
Latitude
0.00001°
Longitude
-22.82627°
Altitude
761.842 km
Speed
7.467 km/s
True Right ascension
23h 34m 29s
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
03:21:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
756.841 km
Perigee altitude
730.344 km
Semi-major axis
7,121.729 km
Eccentricity
0.00186
Inclination
98.5002°
RAAN
353.6225°
Arg. of periapsis
200.6335°
True anomaly
159.4854°
Mean anomaly
159.4106°
Eccentric anomaly
159.44802°
Mean motion
3.61131 °/min
Orbital period
99.69 mins
BSTAR
0.00011834
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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 | 2025-10-26 16:00:32.349Z | 33.505° NE | 2025-10-26 16:04:32.349Z | 93.543° ESE | 29.904° | 2025-10-26 16:08:32.349Z | 159.878° S |
| 6 mins | 2025-10-26 17:40:32.349Z | 335.058° NNW | 2025-10-26 17:43:32.349Z | 284.945° WNW | 22.777° | 2025-10-26 17:46:32.349Z | 243.488° WSW |
| 8 mins | 2025-10-27 03:12:32.349Z | 134.658° SE | 2025-10-27 03:15:32.349Z | 83.418° E | 34.408° | 2025-10-27 03:20:32.349Z | 0.551° NNE |
| 5 mins | 2025-10-27 04:52:32.349Z | 234.503° WSW | 2025-10-27 04:54:32.349Z | 264.172° W | 19.226° | 2025-10-27 04:57:32.349Z | 306.473° NW |
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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