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 26053.58091138 +.00000000 +00000-0 +90465-4 0 00006
2 20480 99.0646 357.7725 0540653 44.1660 320.1314 12.83487145 07
| Epoch (UTC): | 22 February 2026 13:56:30 |
| Eccentricity: | 0.0540653 |
| inclination: | 99.0646° |
| perigee height: | 911 km |
| apogee height: | 1744 km |
| right ascension of ascending node: | 357.7725° |
| argument of perigee: | 44.1660° |
| revolutions per day: | 12.83487145 |
| mean anomaly at epoch: | 320.1314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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