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 52117U 26145.10052925 +.00000000 +00000-0 -25467-3 0 00009
2 52117 53.2127 96.0983 0001243 70.9946 289.1181 15.08856472 04
| Epoch (UTC): | 25 May 2026 02:24:45 |
| Eccentricity: | 0.0001243 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 96.0983° |
| argument of perigee: | 70.9946° |
| revolutions per day: | 15.08856472 |
| mean anomaly at epoch: | 289.1181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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