Showing default

KHALIFASAT, 43676

Orbit data source: Space-Track

KHALIFASAT, 43676 is a payload satellite owned by Rashid Space Ctr (AE) in SSO that was launched on Mon, 29 Oct 2018 UTC via an H-IIA 202 launch vehicle from the Tanegashima Space Center (TNSTA). 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
43676, 2018-084F
Orbit
SSO
Country
Flag of AEAE / UAE
Related business
Manufacturer
MBRSC/SATREC
Mission
Operational Civil Imaging
Bus & Motor
SI-300, Unknown motor
Mass
330 kg wet, 300 kg dry
Launch date (UTC)
2018-10-29 (8 years ago)
Launch vehicle
H-IIA 202
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Hex Cyl + 3 Pan, 1.5 m
Radar Cross Section
2.520 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 KHALIFASAT
1 43676U 18084F   26230.97551410  .00001228  00000-0  10003-3 0  9992
2 43676  98.0879  55.9307 0003915 279.9029  80.1752 15.01504560425195
Epoch: 2026-08-18T23:24Z
TLE epoch observation values (Epoch: 2026-08-18T23:24:44.418Z)
Latitude
-0.00001°
Longitude
97.41001°
Altitude
564.838 km
Speed
7.579 km/s
True Right ascension
03h 43m 43s
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
19:43:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.993 km
Perigee altitude
556.561 km
Semi-major axis
6,937.414 km
Eccentricity
0.00039
Inclination
98.0879°
RAAN
55.9307°
Arg. of periapsis
279.9029°
True anomaly
80.21941°
Mean anomaly
80.1752°
Eccentric anomaly
80.1973°
Mean motion
3.75618 °/min
Orbital period
95.84 mins
BSTAR
0.00010003
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
|