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 31701U 07027A 26010.78640467 0.00000000 00000-0 00000-0 0 02
2 31701 63.3774 9.0894 0449486 23.5863 336.4137 13.40989414 06
| Epoch (UTC): | 10 January 2026 18:52:25 |
| Eccentricity: | 0.0449486 |
| inclination: | 63.3774° |
| perigee height: | 769 km |
| apogee height: | 1442 km |
| right ascension of ascending node: | 9.0894° |
| argument of perigee: | 23.5863° |
| revolutions per day: | 13.40989414 |
| mean anomaly at epoch: | 336.4137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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