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LPNTSAT-001, 68408

Orbit data source: Space-Track

LPNTSAT-001, 68408 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
68408, 2026-065A
Orbit
SSO
Country
Flag of ESAESA
Related business
Manufacturer
GMV
Mission
Operational spacecraft
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
20 kg wet, 20 kg dry
Launch date (UTC)
2026-03-28 (2 weeks ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 LPNTSAT-001
1 68408U 26065A   26101.12192295  .00002168  00000-0  10867-3 0  9998
2 68408  97.4111 343.0283 0015646 234.6093 125.3680 15.18311040  2082
Epoch: 2026-04-11T02:55Z
TLE epoch observation values (Epoch: 2026-04-11T02:55:34.142Z)
Latitude
-0.00006°
Longitude
99.79028°
Altitude
520.284 km
Speed
7.6 km/s
True Right ascension
22h 52m 06s
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
19:56:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
518.687 km
Perigee altitude
497.139 km
Semi-major axis
6,886.05 km
Eccentricity
0.00156
Inclination
97.4111°
RAAN
343.0283°
Arg. of periapsis
234.6093°
True anomaly
125.51404°
Mean anomaly
125.368°
Eccentric anomaly
125.44103°
Mean motion
3.79829 °/min
Orbital period
94.78 mins
BSTAR
0.00010867
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Other satellites on launch #65 in the year 2026 (2026-03-28 UTC)

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