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 60423U 26143.56884767 +.00000000 +00000-0 +00000-0 0 00005
2 60423 62.8072 46.5193 5596833 269.3265 29.7887 1.50428815 07
| Epoch (UTC): | 23 May 2026 13:39:08 |
| Eccentricity: | 0.5596833 |
| inclination: | 62.8072° |
| perigee height: | 7789 km |
| apogee height: | 43804 km |
| right ascension of ascending node: | 46.5193° |
| argument of perigee: | 269.3265° |
| revolutions per day: | 1.50428815 |
| mean anomaly at epoch: | 29.7887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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