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 44884U 19093F 24358.36481924 .00010141 00000-0 97308-3 0 9996
2 44884 97.8232 78.0289 0011629 53.4203 306.8084 14.93237814271495
| Epoch (UTC): | 23 December 2024 08:45:20 |
| Eccentricity: | 0.0011629 |
| inclination: | 97.8232° |
| perigee height: | 580 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 78.0289° |
| argument of perigee: | 53.4203° |
| revolutions per day: | 14.93237814 |
| mean anomaly at epoch: | 306.8084° |
| orbit number at epoch: | 27149 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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