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 66918U 26145.59702139 +.00000000 +00000-0 +52659-4 0 00008
2 66918 50.0044 227.0158 0001054 214.6751 145.4053 13.29325283 06
| Epoch (UTC): | 25 May 2026 14:19:42 |
| Eccentricity: | 0.0001054 |
| inclination: | 50.0044° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 227.0158° |
| argument of perigee: | 214.6751° |
| revolutions per day: | 13.29325283 |
| mean anomaly at epoch: | 145.4053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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