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 46818U 26145.00094523 +.00000000 +00000-0 +40710-3 0 00006
2 46818 97.1990 226.2160 0004311 204.3518 155.7555 15.93789971 07
| Epoch (UTC): | 25 May 2026 00:01:21 |
| Eccentricity: | 0.0004311 |
| inclination: | 97.1990° |
| perigee height: | 289 km |
| apogee height: | 295 km |
| right ascension of ascending node: | 226.2160° |
| argument of perigee: | 204.3518° |
| revolutions per day: | 15.93789971 |
| mean anomaly at epoch: | 155.7555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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