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 46058U 26145.29719013 +.00000000 +00000-0 +96524-5 0 00007
2 46058 53.1585 118.5323 0001415 88.7142 271.4021 15.30192138 06
| Epoch (UTC): | 25 May 2026 07:07:57 |
| Eccentricity: | 0.0001415 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 118.5323° |
| argument of perigee: | 88.7142° |
| revolutions per day: | 15.30192138 |
| mean anomaly at epoch: | 271.4021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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