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 60445U 26145.35063119 +.00000000 +00000-0 +59459-4 0 00004
2 60445 53.1596 219.8163 0001001 72.5345 287.5767 15.34391041 01
| Epoch (UTC): | 25 May 2026 08:24:54 |
| Eccentricity: | 0.0001001 |
| inclination: | 53.1596° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.8163° |
| argument of perigee: | 72.5345° |
| revolutions per day: | 15.34391041 |
| mean anomaly at epoch: | 287.5767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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