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 60255U 26145.45524912 +.00000000 +00000-0 -13317-4 0 00001
2 60255 53.1605 55.7308 0000985 89.9574 270.1540 15.31699130 09
| Epoch (UTC): | 25 May 2026 10:55:33 |
| Eccentricity: | 0.0000985 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 55.7308° |
| argument of perigee: | 89.9574° |
| revolutions per day: | 15.31699130 |
| mean anomaly at epoch: | 270.1540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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