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 43246U 26144.79388617 +.00000000 +00000-0 +00000-0 0 00008
2 43246 54.2138 300.7925 0004375 39.9208 320.0884 1.86228954 00
| Epoch (UTC): | 24 May 2026 19:03:11 |
| Eccentricity: | 0.0004375 |
| inclination: | 54.2138° |
| perigee height: | 21516 km |
| apogee height: | 21540 km |
| right ascension of ascending node: | 300.7925° |
| argument of perigee: | 39.9208° |
| revolutions per day: | 1.86228954 |
| mean anomaly at epoch: | 320.0884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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