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 20480U 26106.50735772 +.00000000 +00000-0 -50053-4 0 00006
2 20480 99.0707 40.8577 0539134 284.3175 69.8663 12.83488909 04
| Epoch (UTC): | 16 April 2026 12:10:35 |
| Eccentricity: | 0.0539134 |
| inclination: | 99.0707° |
| perigee height: | 912 km |
| apogee height: | 1743 km |
| right ascension of ascending node: | 40.8577° |
| argument of perigee: | 284.3175° |
| revolutions per day: | 12.83488909 |
| mean anomaly at epoch: | 69.8663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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