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 46351U 26144.86684007 +.00000000 +00000-0 +75171-3 0 00002
2 46351 53.0414 321.3493 0003836 279.2384 80.8200 15.73656026 07
| Epoch (UTC): | 24 May 2026 20:48:14 |
| Eccentricity: | 0.0003836 |
| inclination: | 53.0414° |
| perigee height: | 346 km |
| apogee height: | 351 km |
| right ascension of ascending node: | 321.3493° |
| argument of perigee: | 279.2384° |
| revolutions per day: | 15.73656026 |
| mean anomaly at epoch: | 80.8200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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