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 63595U 26145.33573000 +.00000000 +00000-0 +66113-3 0 00000
2 63595 43.0036 248.6671 0000953 257.3683 102.7063 15.27585760 06
| Epoch (UTC): | 25 May 2026 08:03:27 |
| Eccentricity: | 0.0000953 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 248.6671° |
| argument of perigee: | 257.3683° |
| revolutions per day: | 15.27585760 |
| mean anomaly at epoch: | 102.7063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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