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 23275.01775090 .00000003 00000-0 -12925-4 0 9991
2 21667 82.9016 97.9169 0020208 331.5734 147.2803 13.75154037611491
| Epoch (UTC): | 02 October 2023 00:25:33 |
| Eccentricity: | 0.0020208 |
| inclination: | 82.9016° |
| perigee height: | 966 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 97.9169° |
| argument of perigee: | 331.5734° |
| revolutions per day: | 13.75154037 |
| mean anomaly at epoch: | 147.2803° |
| orbit number at epoch: | 61149 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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