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 20559U 26044.77326308 +.00000000 +00000-0 +10643-2 0 00002
2 20559 30.7947 283.6690 4127657 199.8805 137.6966 7.31234369 05
| Epoch (UTC): | 13 February 2026 18:33:29 |
| Eccentricity: | 0.4127657 |
| inclination: | 30.7947° |
| perigee height: | 206 km |
| apogee height: | 9462 km |
| right ascension of ascending node: | 283.6690° |
| argument of perigee: | 199.8805° |
| revolutions per day: | 7.31234369 |
| mean anomaly at epoch: | 137.6966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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