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.
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43676 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AE / UAERelated business
Manufacturer
MBRSC/SATREC
Mission
Operational Civil Imaging
Bus & Motor
SI-300, Unknown motor
Mass
330 kg wet, 300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 3 Pan, 1.5 m
Radar Cross Section
2.520 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 KHALIFASAT
1 43676U 18084F 25286.96461666 .00004120 00000-0 33686-3 0 9990
2 43676 98.1014 94.5371 0008177 199.6166 160.4743 14.99930190378841Epoch: 2025-10-13T23:09Z
TLE epoch observation values (Epoch: 2025-10-13T23:09:02.879Z)
Latitude
0°
Longitude
84.51526°
Altitude
575.508 km
Speed
7.57 km/s
True Right ascension
06h 18m 08s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
01:32:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.812 km
Perigee altitude
558.459 km
Semi-major axis
6,942.272 km
Eccentricity
0.00082
Inclination
98.1014°
RAAN
94.5371°
Arg. of periapsis
199.6166°
True anomaly
160.50559°
Mean anomaly
160.4743°
Eccentric anomaly
160.48995°
Mean motion
3.75224 °/min
Orbital period
95.94 mins
BSTAR
0.00033686
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Other satellites on launch #84 in the year 2018 (2018-10-29 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.KHALIFASAT Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-14 10:30:14.921Z | 118.577° SE | 2025-10-14 10:33:14.921Z | 62.25° ENE | 22.59° | 2025-10-14 10:36:14.921Z | 14.19° NNE |
| 4 mins | 2025-10-14 12:06:14.921Z | 228.946° WSW | 2025-10-14 12:08:14.921Z | 272.123° WNW | 21.913° | 2025-10-14 12:10:14.921Z | 308.902° NW |
| 6 mins | 2025-10-14 23:45:14.921Z | 39.86° NE | 2025-10-14 23:47:14.921Z | 87.821° E | 32.527° | 2025-10-14 23:51:14.921Z | 169.63° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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