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 21949U 92023A 24357.63501785 .00000334 00000-0 11675-3 0 9990
2 21949 85.0076 26.4413 0002174 70.3867 289.7560 14.32115282 31514
| Epoch (UTC): | 22 December 2024 15:14:25 |
| Eccentricity: | 0.0002174 |
| inclination: | 85.0076° |
| perigee height: | 783 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 26.4413° |
| argument of perigee: | 70.3867° |
| revolutions per day: | 14.32115282 |
| mean anomaly at epoch: | 289.7560° |
| orbit number at epoch: | 3151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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