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 63718U 26145.50508308 +.00000000 +00000-0 +37562-3 0 00001
2 63718 53.1578 222.5235 0001024 88.6173 271.4946 15.31681804 07
| Epoch (UTC): | 25 May 2026 12:07:19 |
| Eccentricity: | 0.0001024 |
| inclination: | 53.1578° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 222.5235° |
| argument of perigee: | 88.6173° |
| revolutions per day: | 15.31681804 |
| mean anomaly at epoch: | 271.4946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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