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 66000U 26145.57794432 +.00000000 +00000-0 +49719-4 0 00008
2 66000 50.0054 256.7393 0000907 154.3180 205.7737 13.29328370 00
| Epoch (UTC): | 25 May 2026 13:52:14 |
| Eccentricity: | 0.0000907 |
| inclination: | 50.0054° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 256.7393° |
| argument of perigee: | 154.3180° |
| revolutions per day: | 13.29328370 |
| mean anomaly at epoch: | 205.7737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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