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 53968U 26145.53062683 +.00000000 +00000-0 +12573-3 0 00006
2 53968 53.2166 239.0847 0001173 101.1937 258.9187 15.08843751 05
| Epoch (UTC): | 25 May 2026 12:44:06 |
| Eccentricity: | 0.0001173 |
| inclination: | 53.2166° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 239.0847° |
| argument of perigee: | 101.1937° |
| revolutions per day: | 15.08843751 |
| mean anomaly at epoch: | 258.9187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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