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 66905U 26145.39966237 +.00000000 +00000-0 +94174-3 0 00000
2 66905 53.1607 28.2200 0001162 83.8908 276.2225 15.30213693 09
| Epoch (UTC): | 25 May 2026 09:35:30 |
| Eccentricity: | 0.0001162 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 28.2200° |
| argument of perigee: | 83.8908° |
| revolutions per day: | 15.30213693 |
| mean anomaly at epoch: | 276.2225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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