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 25199.31542353 .00000000 00000-0 36956-5 0 9998
2 00016 34.2578 190.6063 2022862 150.6609 222.4595 10.49573298653834
| Epoch (UTC): | 18 July 2025 07:34:12 |
| Eccentricity: | 0.2022862 |
| inclination: | 34.2578° |
| perigee height: | 651 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 190.6063° |
| argument of perigee: | 150.6609° |
| revolutions per day: | 10.49573298 |
| mean anomaly at epoch: | 222.4595° |
| orbit number at epoch: | 65383 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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