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 66557U 26145.64162238 +.00000000 +00000-0 +58383-3 0 00002
2 66557 42.9990 272.9094 0001336 271.6305 88.4393 15.27602291 04
| Epoch (UTC): | 25 May 2026 15:23:56 |
| Eccentricity: | 0.0001336 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 272.9094° |
| argument of perigee: | 271.6305° |
| revolutions per day: | 15.27602291 |
| mean anomaly at epoch: | 88.4393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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