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CH 3 PROPULSION MODULE, 57770

Orbit data source: Space-Track

CH 3 PROPULSION MODULE, 57770 is a payload satellite owned by ISRO (IN) in HEO that was launched on Fri, 14 Jul 2023 UTC via a LVM3 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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Identifier
57770, 2023-098C
Orbit
HEO
Last TLE update
2 days ago
Origin
Manufacturer
ISRO SAC/Banga
Mission
Operational Civil Planetary
Bus & Motor
CH2O, LAE
Mass
2,145 kg wet, 448 kg dry
Launch date (UTC)
2023-07-14 (2 years ago)
Launch vehicle
LVM3
Launch site
Sirharikota (SRI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 10 m
Radar Cross Section
16.757 m²

Expand to show TLE details & history

TLE from 2 days ago
0 CH 3 PROPULSION MODULE
1 57770U 23098C   25166.58879352 -.00002666  00000-0  00000-0 0  9996
2 57770  33.9092   3.2131 4182190 295.7623 357.1016  0.08327353   434
Epoch: 2025-06-15T14:07Z
TLE epoch observation values (Epoch: 2025-06-15T14:07:51.76Z)
Latitude
-30.43736°
Longitude
-174.12767°
Altitude
120,230.797 km
Speed
2.121 km/s
True Right ascension
20h 07m 47s
True Declination
-30° 25' 44"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
16.58943°
Longitude
-86.26815°
Altitude
185,458.235 km
Speed
1.535 km/s
Apparent Right ascension
02h 01m 54s
Apparent Declination
15° 04' 13"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
15:45:22
Azimuth
29.1° NE
Elevation
-29.971°
Doppler factor
1
Orbital elements
Apogee altitude
307,774.735 km
Perigee altitude
122,493.477 km
Semi-major axis
221,512.243 km
Eccentricity
0.41822
Inclination
33.9092°
RAAN
3.2131°
Arg. of periapsis
295.7623°
True anomaly
Unknown
Mean anomaly
357.1016°
Eccentric anomaly
Unknown
Mean motion
0.02082 °/min
Orbital period
17,292.43 mins
BSTAR
0
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Other satellites on launch #98 in the year 2023 (2023-07-14 UTC)

CH 3 PROPULSION MODULE Visibility forecast

Observer location: undefined°, undefined°

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.
811 mins2025-06-17 09:37:00.372Z74.184° E2025-06-17 16:16:00.372Z184.024° SSW43.725°2025-06-17 23:08:00.372Z294.803° NW
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