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 01738U 65093A 24280.76584401 .00000937 00000-0 30523-3 0 9998
2 01738 59.7078 188.0427 0130109 185.3290 174.6372 14.41200872 67225
| Epoch (UTC): | 06 October 2024 18:22:48 |
| Eccentricity: | 0.0130109 |
| inclination: | 59.7078° |
| perigee height: | 662 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 188.0427° |
| argument of perigee: | 185.3290° |
| revolutions per day: | 14.41200872 |
| mean anomaly at epoch: | 174.6372° |
| orbit number at epoch: | 6722 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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