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 28485U 04047A 25198.20879006 .00016817 00000-0 39734-3 0 9991
2 28485 20.5535 189.2583 0005192 67.9346 292.1646 15.39458172134875
| Epoch (UTC): | 17 July 2025 05:00:39 |
| Eccentricity: | 0.0005192 |
| inclination: | 20.5535° |
| perigee height: | 444 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 189.2583° |
| argument of perigee: | 67.9346° |
| revolutions per day: | 15.39458172 |
| mean anomaly at epoch: | 292.1646° |
| orbit number at epoch: | 13487 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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