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 25119.20327871 .00001787 00000-0 21286-3 0 9990
2 44881 97.7934 195.7181 0014020 13.6007 346.5584 14.85504500289930
| Epoch (UTC): | 29 April 2025 04:52:43 |
| Eccentricity: | 0.0014020 |
| inclination: | 97.7934° |
| perigee height: | 602 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 195.7181° |
| argument of perigee: | 13.6007° |
| revolutions per day: | 14.85504500 |
| mean anomaly at epoch: | 346.5584° |
| orbit number at epoch: | 28993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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