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 28352U 04021A 25135.65748491 .00000196 00000-0 13252-3 0 9999
2 28352 70.9981 210.1864 0007106 350.3241 9.7742 14.12070922 78642
| Epoch (UTC): | 15 May 2025 15:46:46 |
| Eccentricity: | 0.0007106 |
| inclination: | 70.9981° |
| perigee height: | 847 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 210.1864° |
| argument of perigee: | 350.3241° |
| revolutions per day: | 14.12070922 |
| mean anomaly at epoch: | 9.7742° |
| orbit number at epoch: | 7864 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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