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 26022.26933612 +.00000000 +00000-0 +13731-2 0 00007
2 31702 63.3141 322.1418 0502532 41.5246 322.2886 14.49742811 05
| Epoch (UTC): | 22 January 2026 06:27:50 |
| Eccentricity: | 0.0502532 |
| inclination: | 63.3141° |
| perigee height: | 369 km |
| apogee height: | 1084 km |
| right ascension of ascending node: | 322.1418° |
| argument of perigee: | 41.5246° |
| revolutions per day: | 14.49742811 |
| mean anomaly at epoch: | 322.2886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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