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 60386U 26145.61142764 +.00000000 +00000-0 +98895-4 0 00008
2 60386 88.9721 282.2648 0018562 86.9245 273.4030 13.51005528 07
| Epoch (UTC): | 25 May 2026 14:40:27 |
| Eccentricity: | 0.0018562 |
| inclination: | 88.9721° |
| perigee height: | 1055 km |
| apogee height: | 1082 km |
| right ascension of ascending node: | 282.2648° |
| argument of perigee: | 86.9245° |
| revolutions per day: | 13.51005528 |
| mean anomaly at epoch: | 273.4030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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