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 14820U 26020.14202038 +.00000000 +00000-0 +67377-4 0 00002
2 14820 82.5427 290.5479 0019091 130.9024 229.3849 14.85920156 08
| Epoch (UTC): | 20 January 2026 03:24:30 |
| Eccentricity: | 0.0019091 |
| inclination: | 82.5427° |
| perigee height: | 597 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 290.5479° |
| argument of perigee: | 130.9024° |
| revolutions per day: | 14.85920156 |
| mean anomaly at epoch: | 229.3849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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