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 25193.70228117 -.00000055 00000-0 -61475-4 0 9999
2 00016 34.2580 206.8461 2022950 126.9449 253.3990 10.49573427653246
| Epoch (UTC): | 12 July 2025 16:51:17 |
| Eccentricity: | 0.2022950 |
| inclination: | 34.2580° |
| perigee height: | 651 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 206.8461° |
| argument of perigee: | 126.9449° |
| revolutions per day: | 10.49573427 |
| mean anomaly at epoch: | 253.3990° |
| orbit number at epoch: | 65324 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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