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 00016U 58002A 25345.68850066 .00000023 00000-0 59027-4 0 9992
2 00016 34.2588 127.2445 2022682 48.7884 327.0289 10.49576844669218
| Epoch (UTC): | 11 December 2025 16:31:26 |
| Eccentricity: | 0.2022682 |
| inclination: | 34.2588° |
| perigee height: | 651 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 127.2445° |
| argument of perigee: | 48.7884° |
| revolutions per day: | 10.49576844 |
| mean anomaly at epoch: | 327.0289° |
| orbit number at epoch: | 66921 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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