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 32062U 26160.11178860 +.00000000 +00000-0 +81692-4 0 00003
2 32062 98.3922 104.9022 0031103 1.5614 13.5849 14.41471799 08
| Epoch (UTC): | 09 June 2026 02:40:58 |
| Eccentricity: | 0.0031103 |
| inclination: | 98.3922° |
| perigee height: | 731 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 104.9022° |
| argument of perigee: | 1.5614° |
| revolutions per day: | 14.41471799 |
| mean anomaly at epoch: | 13.5849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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