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 is defined by the following mean orbital elements,
1 39344U 10057J 25080.47733717 .00009700 00000-0 13761-1 0 9995
2 39344 20.2934 187.8835 6790582 280.2893 15.1127 2.84096532 9829
| Epoch (UTC): | 21 March 2025 11:27:21 |
| Eccentricity: | 0.6790582 |
| inclination: | 20.2934° |
| perigee height: | 380 km |
| apogee height: | 28980 km |
| right ascension of ascending node: | 187.8835° |
| argument of perigee: | 280.2893° |
| revolutions per day: | 2.84096532 |
| mean anomaly at epoch: | 15.1127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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