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 66131U 26145.13004271 +.00000000 +00000-0 +10959-2 0 00002
2 66131 53.1594 44.5809 0001434 90.3955 269.7210 15.30150734 05
| Epoch (UTC): | 25 May 2026 03:07:15 |
| Eccentricity: | 0.0001434 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.5809° |
| argument of perigee: | 90.3955° |
| revolutions per day: | 15.30150734 |
| mean anomaly at epoch: | 269.7210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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