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 44881U 19093C 24357.86886451 .00002237 00000-0 26888-3 0 9993
2 44881 97.8120 70.9765 0015307 67.5605 292.7230 14.84867283271032
| Epoch (UTC): | 22 December 2024 20:51:09 |
| Eccentricity: | 0.0015307 |
| inclination: | 97.8120° |
| perigee height: | 603 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 70.9765° |
| argument of perigee: | 67.5605° |
| revolutions per day: | 14.84867283 |
| mean anomaly at epoch: | 292.7230° |
| orbit number at epoch: | 27103 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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