NEXTSAT-1, 43811
Orbit data source: Space-Track
NEXTSAT-1, 43811 is a payload satellite owned by KAIST (KR) in SSO that was launched on Mon, 03 Dec 2018 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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43811 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SKORRelated business
Manufacturer
SatRec Initiative
Mission
Operational Civil Ast/Tech
Bus & Motor
NEXTSAT, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + Cyl + 1 Pan, 1.0 m
Radar Cross Section
0.908 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 NEXTSAT-1
1 43811U 18099BF 25286.58865580 .00004576 00000-0 31099-3 0 9999
2 43811 97.4446 332.7151 0014651 101.1912 259.0963 15.06752135374729Epoch: 2025-10-13T14:07Z
TLE epoch observation values (Epoch: 2025-10-13T14:07:39.861Z)
Latitude
-0.00006°
Longitude
98.40974°
Altitude
551.138 km
Speed
7.585 km/s
True Right ascension
22h 10m 51s
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
14:28:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
553.258 km
Perigee altitude
532.977 km
Semi-major axis
6,921.255 km
Eccentricity
0.00147
Inclination
97.4446°
RAAN
332.7151°
Arg. of periapsis
101.1912°
True anomaly
258.9315°
Mean anomaly
259.0963°
Eccentric anomaly
259.01389°
Mean motion
3.76935 °/min
Orbital period
95.51 mins
BSTAR
0.00031099
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.NEXTSAT-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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-14 02:59:50.740Z | 154.996° SSE | 2025-10-14 03:03:50.740Z | 49.858° ENE | 40.338° | 2025-10-14 03:06:50.740Z | 356.852° N |
| 6 mins | 2025-10-14 16:11:50.740Z | 5.471° NNE | 2025-10-14 16:14:50.740Z | 256.893° W | 43.098° | 2025-10-14 16:17:50.740Z | 201.169° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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