NOVASAR 1, 43619
Orbit data source: Space-Track
NOVASAR 1, 43619 is a payload satellite owned by SSTL (Astrium) (UK) in SSO that was launched on Sun, 16 Sep 2018 UTC via a PSLV 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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43619 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
UKRelated business
Manufacturer
SSTL (Astrium)
Mission
Operational Commercial Imaging
Bus & Motor
NOVASAR-S, XE
Mass
445 kg wet, 400 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Tri Box, 1.5 m
Radar Cross Section
3.500 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 NOVASAR 1
1 43619U 18071B 25259.72819565 .00000476 00000-0 47165-4 0 9990
2 43619 97.5418 137.5911 0001295 56.6631 303.4714 14.96177752382048Epoch: 2025-09-16T17:28Z
TLE epoch observation values (Epoch: 2025-09-16T17:28:36.104Z)
Latitude
-0.00007°
Longitude
-120.47366°
Altitude
581.277 km
Speed
7.57 km/s
True Right ascension
09h 10m 21s
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
15:39:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.624 km
Perigee altitude
574.822 km
Semi-major axis
6,953.86 km
Eccentricity
0.00013
Inclination
97.5418°
RAAN
137.5911°
Arg. of periapsis
56.6631°
True anomaly
303.45902°
Mean anomaly
303.4714°
Eccentric anomaly
303.46521°
Mean motion
3.74287 °/min
Orbital period
96.18 mins
BSTAR
0.000047165
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Other satellites on launch #71 in the year 2018 (2018-09-16 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.NOVASAR 1 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 | 2025-09-18 03:46:20.032Z | 54.948° ENE | 2025-09-18 03:48:20.032Z | 84.83° E | 15.298° | 2025-09-18 03:50:20.032Z | 118.816° SE |
| 5 mins | 2025-09-18 05:22:20.032Z | 337.776° N | 2025-09-18 05:24:20.032Z | 283.347° WNW | 30.92° | 2025-09-18 05:27:20.032Z | 224.639° SW |
| 6 mins | 2025-09-18 16:09:20.032Z | 179.191° S | 2025-09-18 16:12:20.032Z | 283.169° WNW | 42.252° | 2025-09-18 16:15:20.032Z | 340.398° N |
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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