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 23083.58968202 .00006259 00000-0 14887-2 0 9992
2 26093 100.2010 308.1191 0029717 75.2690 285.1790 14.54037724220221
| Epoch (UTC): | 24 March 2023 14:09:08 |
| Eccentricity: | 0.0029717 |
| inclination: | 100.2010° |
| perigee height: | 691 km |
| apogee height: | 733 km |
| right ascension of ascending node: | 308.1191° |
| argument of perigee: | 75.2690° |
| revolutions per day: | 14.54037724 |
| mean anomaly at epoch: | 285.1790° |
| orbit number at epoch: | 22022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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