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 48962U 21059CM 23275.87775465 .00066766 00000-0 17789-2 0 9999
2 48962 97.6054 55.7579 0005693 252.6739 107.3883 15.37918226125919
| Epoch (UTC): | 02 October 2023 21:03:58 |
| Eccentricity: | 0.0005693 |
| inclination: | 97.6054° |
| perigee height: | 448 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 55.7579° |
| argument of perigee: | 252.6739° |
| revolutions per day: | 15.37918226 |
| mean anomaly at epoch: | 107.3883° |
| orbit number at epoch: | 12591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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