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 63691U 26145.62467745 +.00000000 +00000-0 +26754-4 0 00005
2 63691 86.5075 320.8650 0001442 79.5079 280.6217 13.24408602 06
| Epoch (UTC): | 25 May 2026 14:59:32 |
| Eccentricity: | 0.0001442 |
| inclination: | 86.5075° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 320.8650° |
| argument of perigee: | 79.5079° |
| revolutions per day: | 13.24408602 |
| mean anomaly at epoch: | 280.6217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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