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 66219U 26145.51396084 +.00000000 +00000-0 +37713-3 0 00005
2 66219 53.1595 232.9274 0001294 87.9731 272.1418 15.30194564 07
| Epoch (UTC): | 25 May 2026 12:20:06 |
| Eccentricity: | 0.0001294 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.9274° |
| argument of perigee: | 87.9731° |
| revolutions per day: | 15.30194564 |
| mean anomaly at epoch: | 272.1418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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