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 00053U 26048.22462441 +.00000000 +00000-0 +11581-2 0 00004
2 00053 47.2795 352.3866 0098367 80.4043 280.7844 12.17402198 07
| Epoch (UTC): | 17 February 2026 05:23:27 |
| Eccentricity: | 0.0098367 |
| inclination: | 47.2795° |
| perigee height: | 1525 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 352.3866° |
| argument of perigee: | 80.4043° |
| revolutions per day: | 12.17402198 |
| mean anomaly at epoch: | 280.7844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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