Showing default

EMISAR, 68427

Orbit data source: Space-Track

EMISAR, 68427 is a Romanian 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
68427, 2026-067M
Orbit
SSO
Country
Flag of RORO / ROM
Related business
Manufacturer
RISERO
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
~1 kg wet, ~1 kg dry
Launch date (UTC)
2026-03-30 (4 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: 20 hours ago

TLE from 20 hours ago
0 EMISAR
1 68427U 26067M   26217.42223296  .00006294  00000-0  29424-3 0  9991
2 68427  97.4580 175.3822 0002907 123.5381 236.6132 15.20128760 19422
Epoch: 2026-08-05T10:08Z
TLE epoch observation values (Epoch: 2026-08-05T10:08:00.927Z)
Latitude
-0.00004°
Longitude
69.40148°
Altitude
509.643 km
Speed
7.609 km/s
True Right ascension
11h 41m 31s
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
20:27:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.42 km
Perigee altitude
500.42 km
Semi-major axis
6,880.557 km
Eccentricity
0.00029
Inclination
97.458°
RAAN
175.3822°
Arg. of periapsis
123.5381°
True anomaly
236.58539°
Mean anomaly
236.6132°
Eccentric anomaly
236.59929°
Mean motion
3.80284 °/min
Orbital period
94.67 mins
BSTAR
0.00029424
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
|