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 66201U 26145.54452082 +.00000000 +00000-0 +58250-3 0 00009
2 66201 53.1600 248.0484 0000426 73.3786 286.7263 15.31707117 05
| Epoch (UTC): | 25 May 2026 13:04:06 |
| Eccentricity: | 0.0000426 |
| inclination: | 53.1600° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 248.0484° |
| argument of perigee: | 73.3786° |
| revolutions per day: | 15.31707117 |
| mean anomaly at epoch: | 286.7263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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