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 46146U 26145.44181178 +.00000000 +00000-0 +13541-2 0 00002
2 46146 53.1598 311.9587 0001679 280.1942 79.8871 15.34553686 03
| Epoch (UTC): | 25 May 2026 10:36:12 |
| Eccentricity: | 0.0001679 |
| inclination: | 53.1598° |
| perigee height: | 461 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 311.9587° |
| argument of perigee: | 280.1942° |
| revolutions per day: | 15.34553686 |
| mean anomaly at epoch: | 79.8871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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