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 26106.47318589 +.00000000 +00000-0 +50259-4 0 00001
2 32062 98.3881 52.2169 0031373 158.4388 314.4994 14.41442135 04
| Epoch (UTC): | 16 April 2026 11:21:23 |
| Eccentricity: | 0.0031373 |
| inclination: | 98.3881° |
| perigee height: | 731 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 52.2169° |
| argument of perigee: | 158.4388° |
| revolutions per day: | 14.41442135 |
| mean anomaly at epoch: | 314.4994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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