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 37622U 90081DJ 24358.05163959 .00005589 00000-0 16068-2 0 9998
2 37622 98.3602 32.0478 0034351 173.7481 216.6716 14.44846951253703
| Epoch (UTC): | 23 December 2024 01:14:21 |
| Eccentricity: | 0.0034351 |
| inclination: | 98.3602° |
| perigee height: | 718 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 32.0478° |
| argument of perigee: | 173.7481° |
| revolutions per day: | 14.44846951 |
| mean anomaly at epoch: | 216.6716° |
| orbit number at epoch: | 25370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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