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 39232U 13043A 25106.89296594 0.00057481 00000-0 56588-3 0 09
2 39232 97.9073 170.6909 0518395 57.6797 302.4645 14.80564770 06
| Epoch (UTC): | 16 April 2025 21:25:52 |
| Eccentricity: | 0.0518395 |
| inclination: | 97.9073° |
| perigee height: | 264 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 170.6909° |
| argument of perigee: | 57.6797° |
| revolutions per day: | 14.80564770 |
| mean anomaly at epoch: | 302.4645° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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