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 31702U 26157.01200191 +.00000000 +00000-0 +74578-3 0 00005
2 31702 63.3086 265.0495 0495520 43.6805 320.2393 14.54833949 05
| Epoch (UTC): | 06 June 2026 00:17:16 |
| Eccentricity: | 0.0495520 |
| inclination: | 63.3086° |
| perigee height: | 359 km |
| apogee height: | 1061 km |
| right ascension of ascending node: | 265.0495° |
| argument of perigee: | 43.6805° |
| revolutions per day: | 14.54833949 |
| mean anomaly at epoch: | 320.2393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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