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 38665U 71035E 24351.42697827 .00000428 00000-0 14994-3 0 9998
2 38665 74.0467 237.1710 0029440 133.5656 226.7950 14.37859459102668
| Epoch (UTC): | 16 December 2024 10:14:50 |
| Eccentricity: | 0.0029440 |
| inclination: | 74.0467° |
| perigee height: | 744 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 237.1710° |
| argument of perigee: | 133.5656° |
| revolutions per day: | 14.37859459 |
| mean anomaly at epoch: | 226.7950° |
| orbit number at epoch: | 10266 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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