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 66206U 26145.64117867 +.00000000 +00000-0 +10310-2 0 00008
2 66206 53.1597 232.3063 0001025 85.6443 274.4677 15.34426146 02
| Epoch (UTC): | 25 May 2026 15:23:17 |
| Eccentricity: | 0.0001025 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 232.3063° |
| argument of perigee: | 85.6443° |
| revolutions per day: | 15.34426146 |
| mean anomaly at epoch: | 274.4677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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