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 52100U 26145.30200388 +.00000000 +00000-0 +49545-4 0 00004
2 52100 53.2139 105.1921 0001232 71.6647 288.4479 15.08841774 08
| Epoch (UTC): | 25 May 2026 07:14:53 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 105.1921° |
| argument of perigee: | 71.6647° |
| revolutions per day: | 15.08841774 |
| mean anomaly at epoch: | 288.4479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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