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 52310U 26145.27259067 +.00000000 +00000-0 +86800-4 0 00006
2 52310 53.2135 105.3912 0001268 78.7559 281.3576 15.08838729 04
| Epoch (UTC): | 25 May 2026 06:32:31 |
| Eccentricity: | 0.0001268 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 105.3912° |
| argument of perigee: | 78.7559° |
| revolutions per day: | 15.08838729 |
| mean anomaly at epoch: | 281.3576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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