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 26161.50364933 +.00000000 +00000-0 +24867-3 0 00001
2 31122 98.4128 163.9201 0062670 287.9051 71.5329 14.72988244 04
| Epoch (UTC): | 10 June 2026 12:05:15 |
| Eccentricity: | 0.0062670 |
| inclination: | 98.4128° |
| perigee height: | 607 km |
| apogee height: | 696 km |
| right ascension of ascending node: | 163.9201° |
| argument of perigee: | 287.9051° |
| revolutions per day: | 14.72988244 |
| mean anomaly at epoch: | 71.5329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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