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 46718U 26145.21115985 +.00000000 +00000-0 +16659-2 0 00008
2 46718 53.0446 223.0573 0002967 16.3459 343.7643 15.48116275 04
| Epoch (UTC): | 25 May 2026 05:04:04 |
| Eccentricity: | 0.0002967 |
| inclination: | 53.0446° |
| perigee height: | 420 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 223.0573° |
| argument of perigee: | 16.3459° |
| revolutions per day: | 15.48116275 |
| mean anomaly at epoch: | 343.7643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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