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 26038.80113242 +.00000000 +00000-0 +53708-3 0 00007
2 20682 63.2940 197.9144 0880644 80.4593 289.4737 13.64157426 07
| Epoch (UTC): | 07 February 2026 19:13:37 |
| Eccentricity: | 0.0880644 |
| inclination: | 63.2940° |
| perigee height: | 369 km |
| apogee height: | 1672 km |
| right ascension of ascending node: | 197.9144° |
| argument of perigee: | 80.4593° |
| revolutions per day: | 13.64157426 |
| mean anomaly at epoch: | 289.4737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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