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 23338.42100773 .00001692 00000-0 21415-3 0 9994
2 44881 97.8486 53.9024 0013362 240.0010 119.9878 14.83050055214027
| Epoch (UTC): | 04 December 2023 10:06:15 |
| Eccentricity: | 0.0013362 |
| inclination: | 97.8486° |
| perigee height: | 610 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 53.9024° |
| argument of perigee: | 240.0010° |
| revolutions per day: | 14.83050055 |
| mean anomaly at epoch: | 119.9878° |
| orbit number at epoch: | 21402 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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