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 52615U 26144.65294417 +.00000000 +00000-0 -65111-5 0 00007
2 52615 53.2144 303.1059 0001478 100.1456 259.9703 15.08842598 03
| Epoch (UTC): | 24 May 2026 15:40:14 |
| Eccentricity: | 0.0001478 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 303.1059° |
| argument of perigee: | 100.1456° |
| revolutions per day: | 15.08842598 |
| mean anomaly at epoch: | 259.9703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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