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 31122U 26106.54443795 +.00000000 +00000-0 +20166-3 0 00006
2 31122 98.4146 106.9893 0065779 101.1733 259.6878 14.72759611 07
| Epoch (UTC): | 16 April 2026 13:03:59 |
| Eccentricity: | 0.0065779 |
| inclination: | 98.4146° |
| perigee height: | 606 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 106.9893° |
| argument of perigee: | 101.1733° |
| revolutions per day: | 14.72759611 |
| mean anomaly at epoch: | 259.6878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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