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 60383U 26145.65676448 +.00000000 +00000-0 +11038-3 0 00003
2 60383 88.9693 282.2299 0017263 98.5449 261.7660 13.51008537 08
| Epoch (UTC): | 25 May 2026 15:45:44 |
| Eccentricity: | 0.0017263 |
| inclination: | 88.9693° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 282.2299° |
| argument of perigee: | 98.5449° |
| revolutions per day: | 13.51008537 |
| mean anomaly at epoch: | 261.7660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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