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 16791U 86046A 25188.88555362 .00003975 00000-0 17419-3 0 9993
2 16791 82.4610 29.5021 0017189 108.6152 251.6952 15.21579378128790
| Epoch (UTC): | 07 July 2025 21:15:11 |
| Eccentricity: | 0.0017189 |
| inclination: | 82.4610° |
| perigee height: | 489 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 29.5021° |
| argument of perigee: | 108.6152° |
| revolutions per day: | 15.21579378 |
| mean anomaly at epoch: | 251.6952° |
| orbit number at epoch: | 12879 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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