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 00082U 61004B 25111.02492796 .00000598 00000-0 52345-3 0 9994
2 00082 38.8552 127.5590 1167105 342.7068 13.6840 12.27588871 24910
| Epoch (UTC): | 21 April 2025 00:35:53 |
| Eccentricity: | 0.1167105 |
| inclination: | 38.8552° |
| perigee height: | 633 km |
| apogee height: | 2486 km |
| right ascension of ascending node: | 127.5590° |
| argument of perigee: | 342.7068° |
| revolutions per day: | 12.27588871 |
| mean anomaly at epoch: | 13.6840° |
| orbit number at epoch: | 2491 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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