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 60339U 26145.23542468 +.00000000 +00000-0 +55944-4 0 00007
2 60339 53.1606 80.1479 0001219 81.9353 278.1786 15.30200144 04
| Epoch (UTC): | 25 May 2026 05:39:00 |
| Eccentricity: | 0.0001219 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.1479° |
| argument of perigee: | 81.9353° |
| revolutions per day: | 15.30200144 |
| mean anomaly at epoch: | 278.1786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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