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 60922U 26145.43361595 +.00000000 +00000-0 +36950-4 0 00003
2 60922 53.1595 287.4555 0000885 84.0289 276.0813 15.30192632 06
| Epoch (UTC): | 25 May 2026 10:24:24 |
| Eccentricity: | 0.0000885 |
| inclination: | 53.1595° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.4555° |
| argument of perigee: | 84.0289° |
| revolutions per day: | 15.30192632 |
| mean anomaly at epoch: | 276.0813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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