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 31444U 99025BUG 24356.56369593 .00016015 00000-0 34441-2 0 9998
2 31444 98.9245 263.4911 0082365 87.8079 273.2545 14.56483806925586
| Epoch (UTC): | 21 December 2024 13:31:43 |
| Eccentricity: | 0.0082365 |
| inclination: | 98.9245° |
| perigee height: | 646 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 263.4911° |
| argument of perigee: | 87.8079° |
| revolutions per day: | 14.56483806 |
| mean anomaly at epoch: | 273.2545° |
| orbit number at epoch: | 92558 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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