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 42962U 17061H 24358.12891948 .00000183 00000-0 58261-4 0 9990
2 42962 86.3971 251.3113 0001845 74.8930 285.2470 14.34218129377284
| Epoch (UTC): | 23 December 2024 03:05:38 |
| Eccentricity: | 0.0001845 |
| inclination: | 86.3971° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 251.3113° |
| argument of perigee: | 74.8930° |
| revolutions per day: | 14.34218129 |
| mean anomaly at epoch: | 285.2470° |
| orbit number at epoch: | 37728 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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