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 25189.49447817 .00000351 00000-0 21719-3 0 9998
2 28352 71.0040 97.6721 0010692 278.5871 81.4038 14.12109054 86197
| Epoch (UTC): | 08 July 2025 11:52:02 |
| Eccentricity: | 0.0010692 |
| inclination: | 71.0040° |
| perigee height: | 844 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 97.6721° |
| argument of perigee: | 278.5871° |
| revolutions per day: | 14.12109054 |
| mean anomaly at epoch: | 81.4038° |
| orbit number at epoch: | 8619 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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