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 03230U 68040B 25193.82431123 .00001883 00000-0 14897-3 0 9992
2 03230 74.0310 82.9951 0025655 323.9735 35.9722 15.01214032 53997
| Epoch (UTC): | 12 July 2025 19:47:00 |
| Eccentricity: | 0.0025655 |
| inclination: | 74.0310° |
| perigee height: | 545 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 82.9951° |
| argument of perigee: | 323.9735° |
| revolutions per day: | 15.01214032 |
| mean anomaly at epoch: | 35.9722° |
| orbit number at epoch: | 5399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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