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 44887U 19093J 24358.20012238 .00004814 00000-0 51789-3 0 9993
2 44887 97.8307 77.4719 0014456 67.5188 292.7558 14.88891306271384
| Epoch (UTC): | 23 December 2024 04:48:10 |
| Eccentricity: | 0.0014456 |
| inclination: | 97.8307° |
| perigee height: | 591 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 77.4719° |
| argument of perigee: | 67.5188° |
| revolutions per day: | 14.88891306 |
| mean anomaly at epoch: | 292.7558° |
| orbit number at epoch: | 27138 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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