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 53730U 26144.73667318 +.00000000 +00000-0 +27254-4 0 00003
2 53730 53.2155 272.7633 0001184 89.9422 270.1706 15.08837339 09
| Epoch (UTC): | 24 May 2026 17:40:48 |
| Eccentricity: | 0.0001184 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 272.7633° |
| argument of perigee: | 89.9422° |
| revolutions per day: | 15.08837339 |
| mean anomaly at epoch: | 270.1706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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