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 52646U 26145.10238530 +.00000000 +00000-0 -86819-4 0 00003
2 52646 53.2140 276.1270 0001480 101.1798 258.9361 15.08824920 08
| Epoch (UTC): | 25 May 2026 02:27:26 |
| Eccentricity: | 0.0001480 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 276.1270° |
| argument of perigee: | 101.1798° |
| revolutions per day: | 15.08824920 |
| mean anomaly at epoch: | 258.9361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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