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 53718U 26144.62725390 +.00000000 +00000-0 +18695-4 0 00001
2 53718 53.2160 273.4869 0001232 87.7106 272.4027 15.08840277 05
| Epoch (UTC): | 24 May 2026 15:03:14 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.2160° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 273.4869° |
| argument of perigee: | 87.7106° |
| revolutions per day: | 15.08840277 |
| mean anomaly at epoch: | 272.4027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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