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 60022U 26145.51725125 +.00000000 +00000-0 -43190-4 0 00001
2 60022 53.1608 77.5340 0001162 97.7430 262.3704 15.34369779 09
| Epoch (UTC): | 25 May 2026 12:24:50 |
| Eccentricity: | 0.0001162 |
| inclination: | 53.1608° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 77.5340° |
| argument of perigee: | 97.7430° |
| revolutions per day: | 15.34369779 |
| mean anomaly at epoch: | 262.3704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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