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 00016U 58002A 24254.65597709 .00000827 00000-0 10996-2 0 9991
2 00016 34.2832 9.0157 2025962 278.7557 59.0212 10.49409077621199
| Epoch (UTC): | 10 September 2024 15:44:36 |
| Eccentricity: | 0.2025962 |
| inclination: | 34.2832° |
| perigee height: | 649 km |
| apogee height: | 4220 km |
| right ascension of ascending node: | 9.0157° |
| argument of perigee: | 278.7557° |
| revolutions per day: | 10.49409077 |
| mean anomaly at epoch: | 59.0212° |
| orbit number at epoch: | 62119 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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