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 63943U 26145.51688925 +.00000000 +00000-0 +15005-3 0 00004
2 63943 70.0029 80.6069 0002430 280.1183 79.9702 14.98354448 00
| Epoch (UTC): | 25 May 2026 12:24:19 |
| Eccentricity: | 0.0002430 |
| inclination: | 70.0029° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.6069° |
| argument of perigee: | 280.1183° |
| revolutions per day: | 14.98354448 |
| mean anomaly at epoch: | 79.9702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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