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 60507U 26145.61838535 +.00000000 +00000-0 +17219-3 0 00001
2 60507 97.3018 239.8264 0004530 34.3240 325.8301 15.44671865 09
| Epoch (UTC): | 25 May 2026 14:50:28 |
| Eccentricity: | 0.0004530 |
| inclination: | 97.3018° |
| perigee height: | 429 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 239.8264° |
| argument of perigee: | 34.3240° |
| revolutions per day: | 15.44671865 |
| mean anomaly at epoch: | 325.8301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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