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 66699U 26145.15029502 +.00000000 +00000-0 +35857-3 0 00002
2 66699 97.4203 219.0934 0005445 95.3990 264.7866 15.19785715 02
| Epoch (UTC): | 25 May 2026 03:36:25 |
| Eccentricity: | 0.0005445 |
| inclination: | 97.4203° |
| perigee height: | 503 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 219.0934° |
| argument of perigee: | 95.3990° |
| revolutions per day: | 15.19785715 |
| mean anomaly at epoch: | 264.7866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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