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 52002U 26145.40046053 +.00000000 +00000-0 +26991-3 0 00002
2 52002 53.2144 34.7883 0001374 81.0917 279.0231 15.08838639 09
| Epoch (UTC): | 25 May 2026 09:36:39 |
| Eccentricity: | 0.0001374 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.7883° |
| argument of perigee: | 81.0917° |
| revolutions per day: | 15.08838639 |
| mean anomaly at epoch: | 279.0231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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