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 66399U 26145.50828213 +.00000000 +00000-0 +31185-3 0 00004
2 66399 53.1584 219.5783 0001871 92.1654 267.9563 15.34402659 07
| Epoch (UTC): | 25 May 2026 12:11:55 |
| Eccentricity: | 0.0001871 |
| inclination: | 53.1584° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 219.5783° |
| argument of perigee: | 92.1654° |
| revolutions per day: | 15.34402659 |
| mean anomaly at epoch: | 267.9563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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