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 26021.30363330 +.00000000 +00000-0 +17761-2 0 00002
2 31702 63.3141 325.1179 0502676 41.5007 322.3117 14.49678859 04
| Epoch (UTC): | 21 January 2026 07:17:13 |
| Eccentricity: | 0.0502676 |
| inclination: | 63.3141° |
| perigee height: | 370 km |
| apogee height: | 1084 km |
| right ascension of ascending node: | 325.1179° |
| argument of perigee: | 41.5007° |
| revolutions per day: | 14.49678859 |
| mean anomaly at epoch: | 322.3117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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