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 46805U 26143.07370583 +.00000000 +00000-0 +00000-0 0 00005
2 46805 64.5977 193.3141 0009000 239.0049 120.9752 2.13100163 04
| Epoch (UTC): | 23 May 2026 01:46:08 |
| Eccentricity: | 0.0009000 |
| inclination: | 64.5977° |
| perigee height: | 19107 km |
| apogee height: | 19153 km |
| right ascension of ascending node: | 193.3141° |
| argument of perigee: | 239.0049° |
| revolutions per day: | 2.13100163 |
| mean anomaly at epoch: | 120.9752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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