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 60443U 26145.39692391 +.00000000 +00000-0 +38737-4 0 00002
2 60443 53.1613 220.1056 0001171 89.3891 270.7246 15.34386815 04
| Epoch (UTC): | 25 May 2026 09:31:34 |
| Eccentricity: | 0.0001171 |
| inclination: | 53.1613° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 220.1056° |
| argument of perigee: | 89.3891° |
| revolutions per day: | 15.34386815 |
| mean anomaly at epoch: | 270.7246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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