Showing default

LPNTSAT-001, 68408

Orbit data source: Space-Track

LPNTSAT-001, 68408 is an ESA payload satellite 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.

Loading next visibility...
Identifier
68408, 2026-065A
Orbit
SSO
Country
Flag of ESAESA
Related business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-03-28 (4 days 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: 22 hours ago

TLE from 22 hours ago
0 LPNTSAT-001
1 68408U 26065A   26089.91785105  .00001669  00000-0  84675-4 0  9992
2 68408  97.4140 332.0489 0015416 278.4866  81.4621 15.18225096   382
Epoch: 2026-03-30T22:01Z
TLE epoch observation values (Epoch: 2026-03-30T22:01:42.330Z)
Latitude
-0.00002°
Longitude
173.32002°
Altitude
512.731 km
Speed
7.608 km/s
True Right ascension
22h 08m 11s
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
01:44:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
518.789 km
Perigee altitude
497.557 km
Semi-major axis
6,886.31 km
Eccentricity
0.00154
Inclination
97.414°
RAAN
332.0489°
Arg. of periapsis
278.4866°
True anomaly
81.63685°
Mean anomaly
81.4621°
Eccentric anomaly
81.54947°
Mean motion
3.79807 °/min
Orbital period
94.78 mins
BSTAR
0.000084675
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #65 in the year 2026 (2026-03-28 UTC)

Documentation

Showing up to 5 results
|