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 25196.85376456 .00000040 00000-0 35654-4 0 9993
2 25400 98.7885 144.0481 0009601 348.2665 11.8290 14.25977901405230
| Epoch (UTC): | 15 July 2025 20:29:25 |
| Eccentricity: | 0.0009601 |
| inclination: | 98.7885° |
| perigee height: | 798 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 144.0481° |
| argument of perigee: | 348.2665° |
| revolutions per day: | 14.25977901 |
| mean anomaly at epoch: | 11.8290° |
| orbit number at epoch: | 40523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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