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 15890U 85058B 25188.61128094 .00000342 00000-0 36765-4 0 9994
2 15890 82.5247 25.1433 0018924 230.0486 129.9069 14.85464794140078
| Epoch (UTC): | 07 July 2025 14:40:14 |
| Eccentricity: | 0.0018924 |
| inclination: | 82.5247° |
| perigee height: | 599 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 25.1433° |
| argument of perigee: | 230.0486° |
| revolutions per day: | 14.85464794 |
| mean anomaly at epoch: | 129.9069° |
| orbit number at epoch: | 14007 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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