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 66418U 26145.33413612 +.00000000 +00000-0 +79325-4 0 00009
2 66418 50.0032 17.3943 0000971 54.7527 305.3435 13.29319642 04
| Epoch (UTC): | 25 May 2026 08:01:09 |
| Eccentricity: | 0.0000971 |
| inclination: | 50.0032° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 17.3943° |
| argument of perigee: | 54.7527° |
| revolutions per day: | 13.29319642 |
| mean anomaly at epoch: | 305.3435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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