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 60575U 26145.10127192 +.00000000 +00000-0 +13732-3 0 00006
2 60575 97.6740 220.1509 0004675 121.1784 238.9896 14.96431887 09
| Epoch (UTC): | 25 May 2026 02:25:49 |
| Eccentricity: | 0.0004675 |
| inclination: | 97.6740° |
| perigee height: | 575 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 220.1509° |
| argument of perigee: | 121.1784° |
| revolutions per day: | 14.96431887 |
| mean anomaly at epoch: | 238.9896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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