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 60908U 26145.29120296 +.00000000 +00000-0 +26727-4 0 00003
2 60908 53.1570 113.7854 0000777 92.1701 267.9406 15.69714314 01
| Epoch (UTC): | 25 May 2026 06:59:19 |
| Eccentricity: | 0.0000777 |
| inclination: | 53.1570° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 113.7854° |
| argument of perigee: | 92.1701° |
| revolutions per day: | 15.69714314 |
| mean anomaly at epoch: | 267.9406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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