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 60097U 26145.40437985 +.00000000 +00000-0 +89861-4 0 00009
2 60097 53.1606 40.6627 0001076 94.0616 266.0508 15.30186741 03
| Epoch (UTC): | 25 May 2026 09:42:18 |
| Eccentricity: | 0.0001076 |
| inclination: | 53.1606° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.6627° |
| argument of perigee: | 94.0616° |
| revolutions per day: | 15.30186741 |
| mean anomaly at epoch: | 266.0508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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