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 05118U 71028B 24284.57840630 .00025521 00000-0 78388-3 0 9998
2 05118 81.2472 313.3179 0030431 291.2644 68.5344 15.33114709909098
| Epoch (UTC): | 10 October 2024 13:52:54 |
| Eccentricity: | 0.0030431 |
| inclination: | 81.2472° |
| perigee height: | 446 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 313.3179° |
| argument of perigee: | 291.2644° |
| revolutions per day: | 15.33114709 |
| mean anomaly at epoch: | 68.5344° |
| orbit number at epoch: | 90909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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