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 53914U 26145.51498170 +.00000000 +00000-0 +18749-4 0 00001
2 53914 53.2150 329.1853 0001274 88.4696 271.6442 15.08838260 03
| Epoch (UTC): | 25 May 2026 12:21:34 |
| Eccentricity: | 0.0001274 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 329.1853° |
| argument of perigee: | 88.4696° |
| revolutions per day: | 15.08838260 |
| mean anomaly at epoch: | 271.6442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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