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 66761U 26145.16539050 +.00000000 +00000-0 +40508-3 0 00006
2 66761 97.4189 219.5042 0001612 75.7533 284.3882 15.21859246 07
| Epoch (UTC): | 25 May 2026 03:58:09 |
| Eccentricity: | 0.0001612 |
| inclination: | 97.4189° |
| perigee height: | 499 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 219.5042° |
| argument of perigee: | 75.7533° |
| revolutions per day: | 15.21859246 |
| mean anomaly at epoch: | 284.3882° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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