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 63695U 26145.57929870 +.00000000 +00000-0 +15229-3 0 00009
2 63695 86.4987 320.5724 0001395 84.4320 275.6973 13.24408512 04
| Epoch (UTC): | 25 May 2026 13:54:11 |
| Eccentricity: | 0.0001395 |
| inclination: | 86.4987° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 320.5724° |
| argument of perigee: | 84.4320° |
| revolutions per day: | 13.24408512 |
| mean anomaly at epoch: | 275.6973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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