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 63934U 26145.52540422 +.00000000 +00000-0 +88174-4 0 00002
2 63934 70.0007 80.6480 0002990 271.0364 89.0453 14.98333424 00
| Epoch (UTC): | 25 May 2026 12:36:34 |
| Eccentricity: | 0.0002990 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.6480° |
| argument of perigee: | 271.0364° |
| revolutions per day: | 14.98333424 |
| mean anomaly at epoch: | 89.0453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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