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 63292U 26145.62513264 +.00000000 +00000-0 +36894-3 0 00005
2 63292 97.6474 286.4549 0035806 228.4153 131.4007 15.11311278 02
| Epoch (UTC): | 25 May 2026 15:00:11 |
| Eccentricity: | 0.0035806 |
| inclination: | 97.6474° |
| perigee height: | 507 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 286.4549° |
| argument of perigee: | 228.4153° |
| revolutions per day: | 15.11311278 |
| mean anomaly at epoch: | 131.4007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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