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 22181.21911824 .00000604 00000-0 93933-4 0 9991
2 38340 98.1948 259.8043 0011479 180.0733 180.0477 14.76669201534128
| Epoch (UTC): | 30 June 2022 05:15:31 |
| Eccentricity: | 0.0011479 |
| inclination: | 98.1948° |
| perigee height: | 632 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 259.8043° |
| argument of perigee: | 180.0733° |
| revolutions per day: | 14.76669201 |
| mean anomaly at epoch: | 180.0477° |
| orbit number at epoch: | 53412 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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