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 28480U 04046B 25189.53271755 .00000070 00000-0 41021-4 0 9995
2 28480 98.1932 114.7783 0140147 156.4245 204.3444 14.26841123 73688
| Epoch (UTC): | 08 July 2025 12:47:06 |
| Eccentricity: | 0.0140147 |
| inclination: | 98.1932° |
| perigee height: | 701 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 114.7783° |
| argument of perigee: | 156.4245° |
| revolutions per day: | 14.26841123 |
| mean anomaly at epoch: | 204.3444° |
| orbit number at epoch: | 7368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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