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 16719U 86034A 25193.77598009 .00015076 00000-0 33152-3 0 9996
2 16719 82.5412 322.2944 0007502 84.4838 275.7266 15.43823676143089
| Epoch (UTC): | 12 July 2025 18:37:24 |
| Eccentricity: | 0.0007502 |
| inclination: | 82.5412° |
| perigee height: | 430 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 322.2944° |
| argument of perigee: | 84.4838° |
| revolutions per day: | 15.43823676 |
| mean anomaly at epoch: | 275.7266° |
| orbit number at epoch: | 14308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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