View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 63774U 26145.19877595 +.00000000 +00000-0 +27792-3 0 00009
2 63774 43.0003 329.2189 0000991 280.9296 79.1444 15.27604385 08
| Epoch (UTC): | 25 May 2026 04:46:14 |
| Eccentricity: | 0.0000991 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 329.2189° |
| argument of perigee: | 280.9296° |
| revolutions per day: | 15.27604385 |
| mean anomaly at epoch: | 79.1444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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