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 39173U 13026B 25076.95108032 -.00000188 00000-0 00000-0 0 9991
2 39173 30.7812 345.4669 7634412 132.0701 323.9977 1.10511804 47208
| Epoch (UTC): | 17 March 2025 22:49:33 |
| Eccentricity: | 0.7634412 |
| inclination: | 30.7812° |
| perigee height: | 2970 km |
| apogee height: | 63309 km |
| right ascension of ascending node: | 345.4669° |
| argument of perigee: | 132.0701° |
| revolutions per day: | 1.10511804 |
| mean anomaly at epoch: | 323.9977° |
| orbit number at epoch: | 4720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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