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 60285U 26145.45821990 +.00000000 +00000-0 -18115-4 0 00001
2 60285 53.1597 55.8747 0000950 104.6349 255.4757 15.30189534 04
| Epoch (UTC): | 25 May 2026 10:59:50 |
| Eccentricity: | 0.0000950 |
| inclination: | 53.1597° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 55.8747° |
| argument of perigee: | 104.6349° |
| revolutions per day: | 15.30189534 |
| mean anomaly at epoch: | 255.4757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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