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 66515U 26145.20404203 +.00000000 +00000-0 +27831-3 0 00003
2 66515 41.4727 90.2489 0005482 218.1297 141.9160 15.74279029 09
| Epoch (UTC): | 25 May 2026 04:53:49 |
| Eccentricity: | 0.0005482 |
| inclination: | 41.4727° |
| perigee height: | 343 km |
| apogee height: | 350 km |
| right ascension of ascending node: | 90.2489° |
| argument of perigee: | 218.1297° |
| revolutions per day: | 15.74279029 |
| mean anomaly at epoch: | 141.9160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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