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 21808U 91076D 23340.26947426 0.00005500 00000-0 59203-3 0 09
2 21808 63.3099 85.4184 0901117 57.8937 302.1063 13.46757602 05
| Epoch (UTC): | 06 December 2023 06:28:02 |
| Eccentricity: | 0.0901117 |
| inclination: | 63.3099° |
| perigee height: | 412 km |
| apogee height: | 1756 km |
| right ascension of ascending node: | 85.4184° |
| argument of perigee: | 57.8937° |
| revolutions per day: | 13.46757602 |
| mean anomaly at epoch: | 302.1063° |
| 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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