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 24261.14867115 .00003044 00000-0 36923-3 0 9992
2 44881 97.8223 336.1533 0014697 27.2232 332.9750 14.84236111256684
| Epoch (UTC): | 17 September 2024 03:34:05 |
| Eccentricity: | 0.0014697 |
| inclination: | 97.8223° |
| perigee height: | 606 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 336.1533° |
| argument of perigee: | 27.2232° |
| revolutions per day: | 14.84236111 |
| mean anomaly at epoch: | 332.9750° |
| orbit number at epoch: | 25668 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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