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 66020U 26145.28559233 +.00000000 +00000-0 +69667-3 0 00009
2 66020 53.1598 108.0634 0001333 63.4909 296.6229 15.30203262 00
| Epoch (UTC): | 25 May 2026 06:51:15 |
| Eccentricity: | 0.0001333 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.0634° |
| argument of perigee: | 63.4909° |
| revolutions per day: | 15.30203262 |
| mean anomaly at epoch: | 296.6229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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