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 24720U 97005A 23332.71755628 .00000300 00000-0 13628-2 0 9995
2 24720 31.1683 152.7490 5978907 16.2811 15.9998 3.83767929373841
| Epoch (UTC): | 28 November 2023 17:13:16 |
| Eccentricity: | 0.5978907 |
| inclination: | 31.1683° |
| perigee height: | 551 km |
| apogee height: | 21158 km |
| right ascension of ascending node: | 152.7490° |
| argument of perigee: | 16.2811° |
| revolutions per day: | 3.83767929 |
| mean anomaly at epoch: | 15.9998° |
| orbit number at epoch: | 37384 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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