Key statistics
Satellite TIBA-1 at a glance.
Uptime
2164
Days in orbit
Revolutions
≈ 1.0
Per day
Orbit
GEO
Geostationary Orbit
Inclination
0.1
Latest
Satellite identification and parameters
Extended collection of information and parameters for TIBA-1.
Object identification
Identified? True
Debris? False
Object name: TIBA-1
International designator: 2019-080A
Object number (NORAD): 44800
Object ID (CCSDS): 44800
Country: EGYPT (EGYP)
Current information (Y/N): Y
Orbital parameters
Period: 1436.07 minutes
Inclination: 0.0584 deg
SMA: 42164.203 km
Apoapsis: 35795.983 km
Periapsis: 35776.152 km
RAAN: 342.3813 deg
Eccentricy: 0.00023516
Argument of periapsis: 228.7836 deg
Mean anomaly: 85.4801 deg
Mean motion: 1.00273674 rev/day
Mean motion (dot): 0.00000166 rev/day2
B* drag term: 0.0 1/REarth
Two-line elements (TLE)
Creation date: Oct. 28, 2025, 7:11 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 28, 2025, 2:55 p.m. UTC
TLE line 0: 0 TIBA-1
TLE line 1: 1 44800U 19080A 25301.62190341 .00000166 00000-0 00000-0 0 9994
TLE line 2: 2 44800 0.0584 342.3813 0002352 228.7836 85.4801 1.00273674 21736
Live tracking on map
Real-time ground track for satellite TIBA-1.
In-orbit conjunctions
There are no conjunctions computed for TIBA-1, at the moment. Check back to stay up to date, as we update our databases every day.
Go to all conjunctionsAssociated space launch
TIBA-1 is a geostationary communications satellite for the Government of Egypt developed jointly by Thales Alenia Space (TAS) and Airbus. TAS, the leading partner, designed and built the communications payload, featuring a dual mission in Ka-band for secure and broadband communications. Airbus Defence and Space supplied the Eurostar E3000 platform and assembled and tested the spacecraft. Designed to remain in service in orbit for more than 15 years, TIBA-1 will have a launch mass of 5600 kg and an electric power capability of higher than 9 kW. Inmarsat-5 F5 (Global Xpress-5 or GX-5) is Inmarsat's very high throughput satellite (V-HTS), which will offer services covering the Middle East, Europe and the Indian sub-continent. The payload will be fully integrated into Inmarsat’s current Global Express high-speed network. Inmarsat-5 F5 satellite is based on Thales Alenia Space’s upgraded Spacebus 4000 B2 platform and will be fitted with 72 Ka-band beams. With a specified design life of 16 years, it will weigh 4007 kg at launch and will offer payload power of about 6.8 kW.
TIBA-1 was lifted into orbit during the mission ‘Ariane 5 ECA | TIBA-1 & Inmarsat-5 F5 (Global Xpress-5)’, on board a Ariane 5 ECA space rocket.
The launch took place on Nov. 26, 2019, 9:23 p.m. from Ariane Launch Area 3.
For more information about the launch, click the button.
Ariane 5 ECA | TIBA-1 & Inmarsat-5 F5 (Global Xpress-5)
Agency: N/A
Status: Launch Successful
Launch date: Nov. 26, 2019, 9:23 p.m. UTC
Rocket: Ariane 5 ECA
Launch pad: Ariane Launch Area 3
Location: Guiana Space Centre, French Guiana
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