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 66457U 26145.58126847 +.00000000 +00000-0 +89598-3 0 00002
2 66457 42.9989 222.1344 0001542 272.6921 87.3755 15.27580068 07
| Epoch (UTC): | 25 May 2026 13:57:01 |
| Eccentricity: | 0.0001542 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.1344° |
| argument of perigee: | 272.6921° |
| revolutions per day: | 15.27580068 |
| mean anomaly at epoch: | 87.3755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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