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 63291U 26145.64557604 +.00000000 +00000-0 +42811-3 0 00008
2 63291 97.6503 285.3489 0015047 216.8676 143.1523 15.16246204 05
| Epoch (UTC): | 25 May 2026 15:29:37 |
| Eccentricity: | 0.0015047 |
| inclination: | 97.6503° |
| perigee height: | 507 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 285.3489° |
| argument of perigee: | 216.8676° |
| revolutions per day: | 15.16246204 |
| mean anomaly at epoch: | 143.1523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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