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 26155.26189894 +.00000000 +00000-0 +34379-3 0 00003
2 39427 97.8259 65.3632 0088410 276.8265 82.2895 14.81658641 07
| Epoch (UTC): | 04 June 2026 06:17:08 |
| Eccentricity: | 0.0088410 |
| inclination: | 97.8259° |
| perigee height: | 562 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 65.3632° |
| argument of perigee: | 276.8265° |
| revolutions per day: | 14.81658641 |
| mean anomaly at epoch: | 82.2895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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