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 25342.86261605 .00000946 00000-0 11397-3 0 9990
2 44881 97.7764 54.5808 0013712 359.1045 1.0143 14.86087585323142
| Epoch (UTC): | 08 December 2025 20:42:10 |
| Eccentricity: | 0.0013712 |
| inclination: | 97.7764° |
| perigee height: | 600 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 54.5808° |
| argument of perigee: | 359.1045° |
| revolutions per day: | 14.86087585 |
| mean anomaly at epoch: | 1.0143° |
| orbit number at epoch: | 32314 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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