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 66712U 26144.77234822 +.00000000 +00000-0 +25985-3 0 00009
2 66712 97.4220 218.8805 0004655 74.1676 286.0072 15.20107642 04
| Epoch (UTC): | 24 May 2026 18:32:10 |
| Eccentricity: | 0.0004655 |
| inclination: | 97.4220° |
| perigee height: | 502 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 218.8805° |
| argument of perigee: | 74.1676° |
| revolutions per day: | 15.20107642 |
| mean anomaly at epoch: | 286.0072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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