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 66401U 26145.49355527 +.00000000 +00000-0 +58438-3 0 00009
2 66401 53.1586 219.4857 0001025 72.5076 287.6039 15.34402714 04
| Epoch (UTC): | 25 May 2026 11:50:43 |
| Eccentricity: | 0.0001025 |
| inclination: | 53.1586° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.4857° |
| argument of perigee: | 72.5076° |
| revolutions per day: | 15.34402714 |
| mean anomaly at epoch: | 287.6039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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