LPNTSAT-002, 68409
Orbit data source: Space-Track
LPNTSAT-002, 68409 is a payload satellite owned by ESA (ESA) in SSO that was launched on Sat, 28 Mar 2026 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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68409 intel report (Beta)
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Identifier
Orbit
Country
ESARelated business
Manufacturer
THALAQ
Mission
Operational spacecraft
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
30 kg wet, 30 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LPNTSAT-002
1 68409U 26065B 26102.11027694 .00004285 00000-0 21119-3 0 9993
2 68409 97.4098 343.9950 0012790 225.3499 134.6694 15.18407357 2211Epoch: 2026-04-12T02:38Z
TLE epoch observation values (Epoch: 2026-04-12T02:38:47.927Z)
Latitude
0.00002°
Longitude
103.97536°
Altitude
519.943 km
Speed
7.6 km/s
True Right ascension
22h 55m 58s
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
20:41:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.428 km
Perigee altitude
498.815 km
Semi-major axis
6,885.759 km
Eccentricity
0.00128
Inclination
97.4098°
RAAN
343.995°
Arg. of periapsis
225.3499°
True anomaly
134.77351°
Mean anomaly
134.6694°
Eccentric anomaly
134.72147°
Mean motion
3.79853 °/min
Orbital period
94.77 mins
BSTAR
0.00021119
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Other satellites on launch #65 in the year 2026 (2026-03-28 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.LPNTSAT-002 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-12 15:26:54.438Z | 119.218° SE | 2026-04-12 15:28:54.438Z | 78.04° E | 23.842° | 2026-04-12 15:31:54.438Z | 16.963° NNE |
| 5 mins | 2026-04-13 04:31:54.438Z | 36.794° NE | 2026-04-13 04:33:54.438Z | 84.164° E | 31.878° | 2026-04-13 04:36:54.438Z | 163.401° S |
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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