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 60422U 26141.90624897 +.00000000 +00000-0 +00000-0 0 00006
2 60422 62.8377 46.5123 5599565 269.2591 29.7969 1.50427793 08
| Epoch (UTC): | 21 May 2026 21:44:59 |
| Eccentricity: | 0.5599565 |
| inclination: | 62.8377° |
| perigee height: | 7780 km |
| apogee height: | 43813 km |
| right ascension of ascending node: | 46.5123° |
| argument of perigee: | 269.2591° |
| revolutions per day: | 1.50427793 |
| mean anomaly at epoch: | 29.7969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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