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 43770U 26106.11191145 +.00000000 +00000-0 +25872-3 0 00009
2 43770 97.4440 166.6358 0008725 196.1500 163.9461 15.25373467 03
| Epoch (UTC): | 16 April 2026 02:41:09 |
| Eccentricity: | 0.0008725 |
| inclination: | 97.4440° |
| perigee height: | 484 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 166.6358° |
| argument of perigee: | 196.1500° |
| revolutions per day: | 15.25373467 |
| mean anomaly at epoch: | 163.9461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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