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 39251U 13048C 24280.54504786 .00000081 00000-0 51111-3 0 9992
2 39251 82.4947 11.6203 0018319 122.9613 237.3231 12.42881648501983
| Epoch (UTC): | 06 October 2024 13:04:52 |
| Eccentricity: | 0.0018319 |
| inclination: | 82.4947° |
| perigee height: | 1480 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 11.6203° |
| argument of perigee: | 122.9613° |
| revolutions per day: | 12.42881648 |
| mean anomaly at epoch: | 237.3231° |
| orbit number at epoch: | 50198 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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