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 66188U 26145.57203215 +.00000000 +00000-0 -28326-4 0 00001
2 66188 53.1575 248.2258 0001029 71.3794 288.7318 15.30185081 00
| Epoch (UTC): | 25 May 2026 13:43:43 |
| Eccentricity: | 0.0001029 |
| inclination: | 53.1575° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.2258° |
| argument of perigee: | 71.3794° |
| revolutions per day: | 15.30185081 |
| mean anomaly at epoch: | 288.7318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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