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 63696U 26145.57179111 +.00000000 +00000-0 +11195-3 0 00003
2 63696 86.5015 320.6769 0001523 80.7950 279.3356 13.24408818 04
| Epoch (UTC): | 25 May 2026 13:43:22 |
| Eccentricity: | 0.0001523 |
| inclination: | 86.5015° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 320.6769° |
| argument of perigee: | 80.7950° |
| revolutions per day: | 13.24408818 |
| mean anomaly at epoch: | 279.3356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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