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 20682U 26129.80496978 +.00000000 +00000-0 +42373-3 0 00004
2 20682 63.2957 311.5848 0876991 82.2110 287.7473 13.65494209 07
| Epoch (UTC): | 09 May 2026 19:19:09 |
| Eccentricity: | 0.0876991 |
| inclination: | 63.2957° |
| perigee height: | 367 km |
| apogee height: | 1664 km |
| right ascension of ascending node: | 311.5848° |
| argument of perigee: | 82.2110° |
| revolutions per day: | 13.65494209 |
| mean anomaly at epoch: | 287.7473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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