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 38340U 12025D 25138.78044355 .00004594 00000-0 51271-3 0 9994
2 38340 98.1760 252.8286 0009173 38.3806 321.8061 14.87501227690027
| Epoch (UTC): | 18 May 2025 18:43:50 |
| Eccentricity: | 0.0009173 |
| inclination: | 98.1760° |
| perigee height: | 599 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 252.8286° |
| argument of perigee: | 38.3806° |
| revolutions per day: | 14.87501227 |
| mean anomaly at epoch: | 321.8061° |
| orbit number at epoch: | 69002 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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