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 39420U 26099.08941603 +.00000000 +00000-0 +16367-3 0 00004
2 39420 97.6905 327.7053 0115578 233.9168 125.1294 14.72156544 05
| Epoch (UTC): | 09 April 2026 02:08:45 |
| Eccentricity: | 0.0115578 |
| inclination: | 97.6905° |
| perigee height: | 573 km |
| apogee height: | 735 km |
| right ascension of ascending node: | 327.7053° |
| argument of perigee: | 233.9168° |
| revolutions per day: | 14.72156544 |
| mean anomaly at epoch: | 125.1294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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