NUSAT-24 (KALPANA CHAWIA, 52178 (Decayed)
Orbit data source: Space-Track
NUSAT-24 (KALPANA CHAWIA, 52178 was a payload satellite owned by URUGUS S.A. (AR) in LEO that was launched on Fri, 01 Apr 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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52178 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ARGNRelated business
Manufacturer
URUGUS S.A.
Mission
Decayed Commercial Imaging
Bus & Motor
NEWSAT IV, Unknown motor
Mass
41.5 kg wet, 38.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 NUSAT-24 (KALPANA CHAWIA
1 52178U 22033X 25005.51063736 .11649244 24107-5 29536-3 0 9994
2 52178 97.2255 97.1809 0009765 301.4116 58.6231 16.45268786155023Epoch: 2025-01-05T12:15Z
TLE epoch observation values (Epoch: 2025-01-05T12:15:19.067Z)
Latitude
-0.00007°
Longitude
168.006°
Altitude
151.771 km
Speed
7.817 km/s
True Right ascension
06h 28m 43s
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
19:00:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
154.991 km
Perigee altitude
142.244 km
Semi-major axis
6,526.754 km
Eccentricity
0.00098
Inclination
97.2255°
RAAN
97.1809°
Arg. of periapsis
301.4116°
True anomaly
58.7187°
Mean anomaly
58.6231°
Eccentric anomaly
58.67089°
Mean motion
4.11621 °/min
Orbital period
87.46 mins
BSTAR
0.00029536
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Other satellites on launch #33 in the year 2022 (2022-04-01 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.NUSAT-24 (KALPANA CHAWIA Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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