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 60366U 26145.49059861 +.00000000 +00000-0 +53131-4 0 00001
2 60366 53.1610 313.0517 0000985 82.6571 277.4542 15.30199154 09
| Epoch (UTC): | 25 May 2026 11:46:27 |
| Eccentricity: | 0.0000985 |
| inclination: | 53.1610° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.0517° |
| argument of perigee: | 82.6571° |
| revolutions per day: | 15.30199154 |
| mean anomaly at epoch: | 277.4542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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