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 66189U 26145.56570022 +.00000000 +00000-0 +82492-3 0 00006
2 66189 53.1586 248.1870 0001663 87.4147 272.7044 15.30218079 09
| Epoch (UTC): | 25 May 2026 13:34:36 |
| Eccentricity: | 0.0001663 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.1870° |
| argument of perigee: | 87.4147° |
| revolutions per day: | 15.30218079 |
| mean anomaly at epoch: | 272.7044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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