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 66031U 26145.27942693 +.00000000 +00000-0 +64082-3 0 00002
2 66031 53.1593 108.0135 0001088 98.3702 261.7424 15.34372710 07
| Epoch (UTC): | 25 May 2026 06:42:22 |
| Eccentricity: | 0.0001088 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 108.0135° |
| argument of perigee: | 98.3702° |
| revolutions per day: | 15.34372710 |
| mean anomaly at epoch: | 261.7424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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