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 60413U 26144.98836110 +.00000000 +00000-0 +49221-4 0 00002
2 60413 53.1591 247.3803 0001104 95.3400 264.7729 15.34392405 07
| Epoch (UTC): | 24 May 2026 23:43:14 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 247.3803° |
| argument of perigee: | 95.3400° |
| revolutions per day: | 15.34392405 |
| mean anomaly at epoch: | 264.7729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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