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 25347.11646283 .00000024 00000-0 61113-4 0 9996
2 00016 34.2595 123.1139 2022700 54.8205 322.5537 10.49577067669367
| Epoch (UTC): | 13 December 2025 02:47:42 |
| Eccentricity: | 0.2022700 |
| inclination: | 34.2595° |
| perigee height: | 651 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 123.1139° |
| argument of perigee: | 54.8205° |
| revolutions per day: | 10.49577067 |
| mean anomaly at epoch: | 322.5537° |
| orbit number at epoch: | 66936 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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