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 53777U 26145.39356613 +.00000000 +00000-0 +53348-4 0 00003
2 53777 53.2140 289.9384 0001277 88.9790 271.1348 15.08835239 07
| Epoch (UTC): | 25 May 2026 09:26:44 |
| Eccentricity: | 0.0001277 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 289.9384° |
| argument of perigee: | 88.9790° |
| revolutions per day: | 15.08835239 |
| mean anomaly at epoch: | 271.1348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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