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 44909U 19096E 23334.12420119 .00000045 00000-0 13210-3 0 9995
2 44909 82.5228 237.6725 0217736 158.7399 202.2924 12.79724075183439
| Epoch (UTC): | 30 November 2023 02:58:50 |
| Eccentricity: | 0.0217736 |
| inclination: | 82.5228° |
| perigee height: | 1174 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 237.6725° |
| argument of perigee: | 158.7399° |
| revolutions per day: | 12.79724075 |
| mean anomaly at epoch: | 202.2924° |
| orbit number at epoch: | 18343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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