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 25338.88519559 -.00000059 00000-0 -62534-5 0 9999
2 28352 71.0087 145.5735 0009210 49.8942 310.2985 14.12176240107287
| Epoch (UTC): | 04 December 2025 21:14:40 |
| Eccentricity: | 0.0009210 |
| inclination: | 71.0087° |
| perigee height: | 845 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 145.5735° |
| argument of perigee: | 49.8942° |
| revolutions per day: | 14.12176240 |
| mean anomaly at epoch: | 310.2985° |
| orbit number at epoch: | 10728 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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