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 66904U 26145.58335647 +.00000000 +00000-0 +16607-2 0 00009
2 66904 53.1590 26.9413 0000903 95.8922 51.9132 15.30169810 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000903 |
| inclination: | 53.1590° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 26.9413° |
| argument of perigee: | 95.8922° |
| revolutions per day: | 15.30169810 |
| mean anomaly at epoch: | 51.9132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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