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 60355U 26145.18185655 +.00000000 +00000-0 +30685-4 0 00005
2 60355 53.1620 313.9722 0001366 89.5385 270.5773 15.30192996 05
| Epoch (UTC): | 25 May 2026 04:21:52 |
| Eccentricity: | 0.0001366 |
| inclination: | 53.1620° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.9722° |
| argument of perigee: | 89.5385° |
| revolutions per day: | 15.30192996 |
| mean anomaly at epoch: | 270.5773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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