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 23090.35368900 .00000018 00000-0 28686-4 0 9992
2 44909 82.5241 39.6552 0217802 9.2639 351.2380 12.79719548152259
| Epoch (UTC): | 31 March 2023 08:29:18 |
| Eccentricity: | 0.0217802 |
| inclination: | 82.5241° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 39.6552° |
| argument of perigee: | 9.2639° |
| revolutions per day: | 12.79719548 |
| mean anomaly at epoch: | 351.2380° |
| orbit number at epoch: | 15225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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