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 66410U 26145.10671046 +.00000000 +00000-0 +11042-3 0 00004
2 66410 98.2541 211.8524 0015050 49.5268 310.7236 14.50169480 06
| Epoch (UTC): | 25 May 2026 02:33:39 |
| Eccentricity: | 0.0015050 |
| inclination: | 98.2541° |
| perigee height: | 714 km |
| apogee height: | 736 km |
| right ascension of ascending node: | 211.8524° |
| argument of perigee: | 49.5268° |
| revolutions per day: | 14.50169480 |
| mean anomaly at epoch: | 310.7236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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