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 66203U 26145.56464206 +.00000000 +00000-0 +46542-3 0 00005
2 66203 53.1586 248.1738 0000517 57.9462 302.1588 15.30200769 06
| Epoch (UTC): | 25 May 2026 13:33:05 |
| Eccentricity: | 0.0000517 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.1738° |
| argument of perigee: | 57.9462° |
| revolutions per day: | 15.30200769 |
| mean anomaly at epoch: | 302.1588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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