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 25196.36627754 -.00000040 00000-0 -44926-4 0 9990
2 00016 34.2575 199.1392 2022899 138.1997 239.2161 10.49573276653528
| Epoch (UTC): | 15 July 2025 08:47:26 |
| Eccentricity: | 0.2022899 |
| inclination: | 34.2575° |
| perigee height: | 651 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 199.1392° |
| argument of perigee: | 138.1997° |
| revolutions per day: | 10.49573276 |
| mean anomaly at epoch: | 239.2161° |
| orbit number at epoch: | 65352 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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