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 66658U 26145.09012917 +.00000000 +00000-0 +34042-3 0 00007
2 66658 97.7476 74.8261 0014526 92.6288 267.6595 14.94116025 07
| Epoch (UTC): | 25 May 2026 02:09:47 |
| Eccentricity: | 0.0014526 |
| inclination: | 97.7476° |
| perigee height: | 575 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 74.8261° |
| argument of perigee: | 92.6288° |
| revolutions per day: | 14.94116025 |
| mean anomaly at epoch: | 267.6595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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