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 52600U 26145.43173778 +.00000000 +00000-0 +13944-3 0 00008
2 52600 53.2160 294.6090 0001357 91.8876 268.2271 15.08833099 01
| Epoch (UTC): | 25 May 2026 10:21:42 |
| Eccentricity: | 0.0001357 |
| inclination: | 53.2160° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 294.6090° |
| argument of perigee: | 91.8876° |
| revolutions per day: | 15.08833099 |
| mean anomaly at epoch: | 268.2271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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