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 39427U 26106.90433184 +.00000000 +00000-0 +13074-3 0 00003
2 39427 97.8282 18.1125 0092037 74.2310 286.9029 14.81400498 04
| Epoch (UTC): | 16 April 2026 21:42:14 |
| Eccentricity: | 0.0092037 |
| inclination: | 97.8282° |
| perigee height: | 560 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 18.1125° |
| argument of perigee: | 74.2310° |
| revolutions per day: | 14.81400498 |
| mean anomaly at epoch: | 286.9029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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