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 51810U 26144.97818965 +.00000000 +00000-0 +30071-4 0 00003
2 51810 53.2134 346.8690 0001056 67.7899 292.3205 15.08842303 06
| Epoch (UTC): | 24 May 2026 23:28:35 |
| Eccentricity: | 0.0001056 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 346.8690° |
| argument of perigee: | 67.7899° |
| revolutions per day: | 15.08842303 |
| mean anomaly at epoch: | 292.3205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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