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 66851U 26044.54303220 +.00000000 +00000-0 +65480-3 0 00000
2 66851 43.0022 119.7532 0001532 270.7111 89.3566 15.27577488 08
| Epoch (UTC): | 13 February 2026 13:01:57 |
| Eccentricity: | 0.0001532 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 119.7532° |
| argument of perigee: | 270.7111° |
| revolutions per day: | 15.27577488 |
| mean anomaly at epoch: | 89.3566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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