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 66155U 26145.50601374 +.00000000 +00000-0 +31014-3 0 00002
2 66155 53.1600 64.9968 0001242 118.7353 241.3775 15.34400889 00
| Epoch (UTC): | 25 May 2026 12:08:39 |
| Eccentricity: | 0.0001242 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 64.9968° |
| argument of perigee: | 118.7353° |
| revolutions per day: | 15.34400889 |
| mean anomaly at epoch: | 241.3775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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