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 data is extracted from the following two-line orbital elements,
1 26906U 01040B 21011.74092364 0.00000000 00000-0 00000-0 0 01
2 26906 63.4452 225.5006 0460516 339.6670 20.3422 13.44070581 01
| Epoch (UTC): | 11 January 2021 17:46:55 |
| Eccentricity: | 0.0460516 |
| inclination: | 63.4452° |
| perigee height: | 750 km |
| apogee height: | 1438 km |
| right ascension of ascending node: | 225.5006° |
| argument of perigee: | 339.6670° |
| revolutions per day: | 13.44070581 |
| mean anomaly at epoch: | 20.3422° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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