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 63935U 26145.23334579 +.00000000 +00000-0 +30607-3 0 00002
2 63935 70.0007 81.6309 0003141 267.9695 92.1105 14.98338155 07
| Epoch (UTC): | 25 May 2026 05:36:01 |
| Eccentricity: | 0.0003141 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.6309° |
| argument of perigee: | 267.9695° |
| revolutions per day: | 14.98338155 |
| mean anomaly at epoch: | 92.1105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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