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 39352U 10057S 25277.16999493 -.00000360 00000-0 -68511-2 0 9992
2 39352 20.4910 244.4583 7216386 237.9885 280.4415 2.18272380 95433
| Epoch (UTC): | 04 October 2025 04:04:47 |
| Eccentricity: | 0.7216386 |
| inclination: | 20.4910° |
| perigee height: | 610 km |
| apogee height: | 36841 km |
| right ascension of ascending node: | 244.4583° |
| argument of perigee: | 237.9885° |
| revolutions per day: | 2.18272380 |
| mean anomaly at epoch: | 280.4415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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