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 26960U 01049D 23154.54220341 .00006118 00000-0 32022-3 0 9991
2 26960 97.7828 185.3282 0045284 317.5784 42.1950 15.15330041182389
| Epoch (UTC): | 03 June 2023 13:00:46 |
| Eccentricity: | 0.0045284 |
| inclination: | 97.7828° |
| perigee height: | 489 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 185.3282° |
| argument of perigee: | 317.5784° |
| revolutions per day: | 15.15330041 |
| mean anomaly at epoch: | 42.1950° |
| orbit number at epoch: | 18238 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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