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 66873U 26044.60969988 +.00000000 +00000-0 +70595-3 0 00003
2 66873 43.0025 119.3861 0001922 262.0949 97.9685 15.27582573 00
| Epoch (UTC): | 13 February 2026 14:37:58 |
| Eccentricity: | 0.0001922 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 119.3861° |
| argument of perigee: | 262.0949° |
| revolutions per day: | 15.27582573 |
| mean anomaly at epoch: | 97.9685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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