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 66062U 26145.26653763 +.00000000 +00000-0 +47455-3 0 00007
2 66062 53.1601 249.7258 0001850 87.4285 272.6928 15.30181493 04
| Epoch (UTC): | 25 May 2026 06:23:48 |
| Eccentricity: | 0.0001850 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 249.7258° |
| argument of perigee: | 87.4285° |
| revolutions per day: | 15.30181493 |
| mean anomaly at epoch: | 272.6928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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