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 52868U 26144.96759000 +.00000000 +00000-0 +61050-4 0 00001
2 52868 53.2143 41.7255 0001291 90.1408 269.9732 15.08839959 03
| Epoch (UTC): | 24 May 2026 23:13:19 |
| Eccentricity: | 0.0001291 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 41.7255° |
| argument of perigee: | 90.1408° |
| revolutions per day: | 15.08839959 |
| mean anomaly at epoch: | 269.9732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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