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 60201U 26145.52902818 +.00000000 +00000-0 +25022-4 0 00000
2 60201 53.1612 325.3315 0001013 95.4638 264.6478 15.30192789 03
| Epoch (UTC): | 25 May 2026 12:41:48 |
| Eccentricity: | 0.0001013 |
| inclination: | 53.1612° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 325.3315° |
| argument of perigee: | 95.4638° |
| revolutions per day: | 15.30192789 |
| mean anomaly at epoch: | 264.6478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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