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 28647U 05016B 25198.30610816 .00009888 00000-0 29181-3 0 9996
2 28647 57.0003 171.1443 0069236 292.3552 67.0170 15.33332130340843
| Epoch (UTC): | 17 July 2025 07:20:47 |
| Eccentricity: | 0.0069236 |
| inclination: | 57.0003° |
| perigee height: | 418 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 171.1443° |
| argument of perigee: | 292.3552° |
| revolutions per day: | 15.33332130 |
| mean anomaly at epoch: | 67.0170° |
| orbit number at epoch: | 34084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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