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 26019.24852352 +.00000000 +00000-0 +22297-3 0 00004
2 20465 82.4676 96.1316 0010836 138.4317 221.7739 15.10835702 06
| Epoch (UTC): | 19 January 2026 05:57:52 |
| Eccentricity: | 0.0010836 |
| inclination: | 82.4676° |
| perigee height: | 526 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 96.1316° |
| argument of perigee: | 138.4317° |
| revolutions per day: | 15.10835702 |
| mean anomaly at epoch: | 221.7739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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