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 66218U 26145.51606988 +.00000000 +00000-0 +37536-3 0 00004
2 66218 53.1590 232.9409 0001267 90.1864 269.9282 15.30201324 00
| Epoch (UTC): | 25 May 2026 12:23:08 |
| Eccentricity: | 0.0001267 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.9409° |
| argument of perigee: | 90.1864° |
| revolutions per day: | 15.30201324 |
| mean anomaly at epoch: | 269.9282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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