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 46702U 26145.50107571 +.00000000 +00000-0 +11498-2 0 00001
2 46702 53.1560 218.6693 0004067 340.7881 19.2969 15.36571462 00
| Epoch (UTC): | 25 May 2026 12:01:32 |
| Eccentricity: | 0.0004067 |
| inclination: | 53.1560° |
| perigee height: | 453 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 218.6693° |
| argument of perigee: | 340.7881° |
| revolutions per day: | 15.36571462 |
| mean anomaly at epoch: | 19.2969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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