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 20465U 26017.92390942 +.00000000 +00000-0 +19351-3 0 00006
2 20465 82.4682 97.4354 0010692 143.2212 216.9753 15.10826292 03
| Epoch (UTC): | 17 January 2026 22:10:25 |
| Eccentricity: | 0.0010692 |
| inclination: | 82.4682° |
| perigee height: | 526 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 97.4354° |
| argument of perigee: | 143.2212° |
| revolutions per day: | 15.10826292 |
| mean anomaly at epoch: | 216.9753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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