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 62060U 26145.17857110 +.00000000 +00000-0 +19591-2 0 00002
2 62060 53.1565 54.4398 0000941 109.4467 250.6653 15.69790094 06
| Epoch (UTC): | 25 May 2026 04:17:08 |
| Eccentricity: | 0.0000941 |
| inclination: | 53.1565° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 54.4398° |
| argument of perigee: | 109.4467° |
| revolutions per day: | 15.69790094 |
| mean anomaly at epoch: | 250.6653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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