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 66407U 26145.21407356 +.00000000 +00000-0 +62768-3 0 00004
2 66407 53.1587 220.5804 0001211 74.4693 285.6443 15.34406297 06
| Epoch (UTC): | 25 May 2026 05:08:15 |
| Eccentricity: | 0.0001211 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 220.5804° |
| argument of perigee: | 74.4693° |
| revolutions per day: | 15.34406297 |
| mean anomaly at epoch: | 285.6443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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