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 21667U 91059B 24276.63637274 .00000254 00000-0 24936-3 0 9993
2 21667 82.9098 184.8411 0021670 29.5763 25.6229 13.75206299661615
| Epoch (UTC): | 02 October 2024 15:16:22 |
| Eccentricity: | 0.0021670 |
| inclination: | 82.9098° |
| perigee height: | 965 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 184.8411° |
| argument of perigee: | 29.5763° |
| revolutions per day: | 13.75206299 |
| mean anomaly at epoch: | 25.6229° |
| orbit number at epoch: | 66161 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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