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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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Identifier
68409, 2026-065B
Orbit
SSO
Country
Flag of ESAESA
Related business
Manufacturer
THALAQ
Mission
Operational spacecraft
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
30 kg wet, 30 kg dry
Launch date (UTC)
2026-03-28 (3 months ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.4 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 LPNTSAT-002
1 68409U 26065B   26171.22125135  .00005806  00000-0  27781-3 0  9991
2 68409  97.4001  51.6966 0013664 356.9524   3.1625 15.19276108 12704
Epoch: 2026-06-20T05:18Z
TLE epoch observation values (Epoch: 2026-06-20T05:18:36.116Z)
Latitude
-0.00005°
Longitude
63.60714°
Altitude
501.72 km
Speed
7.619 km/s
True Right ascension
03h 26m 47s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:23:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.399 km
Perigee altitude
495.589 km
Semi-major axis
6,883.131 km
Eccentricity
0.00137
Inclination
97.4001°
RAAN
51.6966°
Arg. of periapsis
356.9524°
True anomaly
3.17115°
Mean anomaly
3.1625°
Eccentric anomaly
3.16682°
Mean motion
3.8007 °/min
Orbital period
94.72 mins
BSTAR
0.00027781
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Other satellites on launch #65 in the year 2026 (2026-03-28 UTC)

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