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 31793U 26161.60550948 +.00000000 +00000-0 +18227-3 0 00002
2 31793 70.9763 337.0643 0002216 259.0559 164.2324 14.14851547 01
| Epoch (UTC): | 10 June 2026 14:31:56 |
| Eccentricity: | 0.0002216 |
| inclination: | 70.9763° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 337.0643° |
| argument of perigee: | 259.0559° |
| revolutions per day: | 14.14851547 |
| mean anomaly at epoch: | 164.2324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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