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 60417U 26145.54101117 +.00000000 +00000-0 +39976-4 0 00007
2 60417 53.1597 245.1422 0001147 80.6822 279.4311 15.34389060 05
| Epoch (UTC): | 25 May 2026 12:59:03 |
| Eccentricity: | 0.0001147 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 245.1422° |
| argument of perigee: | 80.6822° |
| revolutions per day: | 15.34389060 |
| mean anomaly at epoch: | 279.4311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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