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 60441U 26145.61959626 +.00000000 +00000-0 -42567-5 0 00000
2 60441 53.1605 218.6529 0001079 71.5049 288.6071 15.34389222 04
| Epoch (UTC): | 25 May 2026 14:52:13 |
| Eccentricity: | 0.0001079 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 218.6529° |
| argument of perigee: | 71.5049° |
| revolutions per day: | 15.34389222 |
| mean anomaly at epoch: | 288.6071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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