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 00012U 59001B 24256.48768028 .00005511 00000-0 32002-2 0 9991
2 00012 32.9116 327.9909 1654198 304.9484 40.6452 11.47095363457457
| Epoch (UTC): | 12 September 2024 11:42:15 |
| Eccentricity: | 0.1654198 |
| inclination: | 32.9116° |
| perigee height: | 553 km |
| apogee height: | 3300 km |
| right ascension of ascending node: | 327.9909° |
| argument of perigee: | 304.9484° |
| revolutions per day: | 11.47095363 |
| mean anomaly at epoch: | 40.6452° |
| orbit number at epoch: | 45745 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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