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 66268U 26145.58714083 +.00000000 +00000-0 +29403-3 0 00006
2 66268 53.1590 194.5035 0001183 81.6544 278.4591 15.30202086 04
| Epoch (UTC): | 25 May 2026 14:05:28 |
| Eccentricity: | 0.0001183 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 194.5035° |
| argument of perigee: | 81.6544° |
| revolutions per day: | 15.30202086 |
| mean anomaly at epoch: | 278.4591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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