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 23335.18244010 .00002052 00000-0 25840-3 0 9994
2 44881 97.8489 50.7222 0013270 251.5576 108.4195 14.83036099213540
| Epoch (UTC): | 01 December 2023 04:22:42 |
| Eccentricity: | 0.0013270 |
| inclination: | 97.8489° |
| perigee height: | 610 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 50.7222° |
| argument of perigee: | 251.5576° |
| revolutions per day: | 14.83036099 |
| mean anomaly at epoch: | 108.4195° |
| orbit number at epoch: | 21354 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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