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 18959U 88020B 25163.44720986 .00000349 00000-0 37687-4 0 9998
2 18959 82.5375 63.0622 0014981 226.1501 133.8478 14.85360788 13168
| Epoch (UTC): | 12 June 2025 10:43:58 |
| Eccentricity: | 0.0014981 |
| inclination: | 82.5375° |
| perigee height: | 602 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 63.0622° |
| argument of perigee: | 226.1501° |
| revolutions per day: | 14.85360788 |
| mean anomaly at epoch: | 133.8478° |
| orbit number at epoch: | 1316 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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