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 38109U 12014A 25170.92605152 0.00000000 00000-0 00000-0 0 07
2 38109 123.0033 71.6534 0009731 59.1818 300.8181 13.41423166 05
| Epoch (UTC): | 19 June 2025 22:13:30 |
| Eccentricity: | 0.0009731 |
| inclination: | 123.0033° |
| perigee height: | 1097 km |
| apogee height: | 1111 km |
| right ascension of ascending node: | 71.6534° |
| argument of perigee: | 59.1818° |
| revolutions per day: | 13.41423166 |
| mean anomaly at epoch: | 300.8181° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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