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 26093U 00004L 21023.67987703 .00000282 00000-0 85201-4 0 9991
2 26093 100.2003 69.8129 0030376 200.7998 159.1957 14.51987358105821
| Epoch (UTC): | 23 January 2021 16:19:01 |
| Eccentricity: | 0.0030376 |
| inclination: | 100.2003° |
| perigee height: | 697 km |
| apogee height: | 741 km |
| right ascension of ascending node: | 69.8129° |
| argument of perigee: | 200.7998° |
| revolutions per day: | 14.51987358 |
| mean anomaly at epoch: | 159.1957° |
| orbit number at epoch: | 10582 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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