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 41459U 16025D 24126.07714411 .16156611 31653-5 27264-3 0 9991
2 41459 98.0991 14.5477 0007120 232.8921 127.1731 16.47786158442898
| Epoch (UTC): | 05 May 2024 01:51:05 |
| Eccentricity: | 0.0007120 |
| inclination: | 98.0991° |
| perigee height: | 140 km |
| apogee height: | 150 km |
| right ascension of ascending node: | 14.5477° |
| argument of perigee: | 232.8921° |
| revolutions per day: | 16.47786158 |
| mean anomaly at epoch: | 127.1731° |
| orbit number at epoch: | 44289 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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