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 51724U 26145.54489103 +.00000000 +00000-0 +18655-4 0 00003
2 51724 53.2140 344.1039 0001498 92.4817 267.6347 15.08837705 02
| Epoch (UTC): | 25 May 2026 13:04:38 |
| Eccentricity: | 0.0001498 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 344.1039° |
| argument of perigee: | 92.4817° |
| revolutions per day: | 15.08837705 |
| mean anomaly at epoch: | 267.6347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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