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 25400U 98043G 25191.59124518 .00000012 00000-0 23691-4 0 9996
2 25400 98.7885 138.7697 0009911 3.4746 356.6501 14.25977004404488
| Epoch (UTC): | 10 July 2025 14:11:23 |
| Eccentricity: | 0.0009911 |
| inclination: | 98.7885° |
| perigee height: | 798 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 138.7697° |
| argument of perigee: | 3.4746° |
| revolutions per day: | 14.25977004 |
| mean anomaly at epoch: | 356.6501° |
| orbit number at epoch: | 40448 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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