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 52101U 26145.18059208 +.00000000 +00000-0 +57720-5 0 00009
2 52101 53.2136 105.9318 0001673 79.8239 280.2941 15.08838310 06
| Epoch (UTC): | 25 May 2026 04:20:03 |
| Eccentricity: | 0.0001673 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 105.9318° |
| argument of perigee: | 79.8239° |
| revolutions per day: | 15.08838310 |
| mean anomaly at epoch: | 280.2941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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