Showing default

FEMTO-1, 68419

Orbit data source: Space-Track

FEMTO-1, 68419 is a Bulgarian payload satellite in SSO that was launched on Mon, 30 Mar 2026 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.

Loading next visibility...
Identifier
68419, 2026-067D
Orbit
SSO
Country
Flag of BGBG / BGR
Related business
Manufacturer
Endurosat
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 1U?, Unknown motor
Mass
~1 kg wet, ~1 kg dry
Launch date (UTC)
2026-03-30 (6 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 4 hours ago

TLE from 4 hours ago
0 FEMTO-1
1 68419U 26067D   26263.61526295  .00002094  00000-0  10217-3 0  9993
2 68419  97.4647 220.9549 0000798  19.6235 340.5031 15.19403883 26431
Epoch: 2026-09-20T14:45Z
TLE epoch observation values (Epoch: 2026-09-20T14:45:58.718Z)
Latitude
0.00003°
Longitude
-0.04666°
Altitude
510.211 km
Speed
7.609 km/s
True Right ascension
14h 43m 49s
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
11:57:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.159 km
Perigee altitude
504.061 km
Semi-major axis
6,882.747 km
Eccentricity
0.00008
Inclination
97.4647°
RAAN
220.9549°
Arg. of periapsis
19.6235°
True anomaly
340.50005°
Mean anomaly
340.5031°
Eccentric anomaly
340.50157°
Mean motion
3.80102 °/min
Orbital period
94.71 mins
BSTAR
0.00010217
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...

Documentation

Showing up to 5 results
|