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 66416U 26144.91650734 +.00000000 +00000-0 +93071-4 0 00002
2 66416 50.0068 19.2553 0000940 62.5987 297.4980 13.29319490 09
| Epoch (UTC): | 24 May 2026 21:59:46 |
| Eccentricity: | 0.0000940 |
| inclination: | 50.0068° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 19.2553° |
| argument of perigee: | 62.5987° |
| revolutions per day: | 13.29319490 |
| mean anomaly at epoch: | 297.4980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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