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 16275U 85109C 25349.90316666 -.00000281 00000-0 00000-0 0 9996
2 16275 13.5072 341.4513 0006645 297.2273 74.3108 0.99944223 44705
| Epoch (UTC): | 15 December 2025 21:40:33 |
| Eccentricity: | 0.0006645 |
| inclination: | 13.5072° |
| perigee height: | 35850 km |
| apogee height: | 35906 km |
| right ascension of ascending node: | 341.4513° |
| argument of perigee: | 297.2273° |
| revolutions per day: | 0.99944223 |
| mean anomaly at epoch: | 74.3108° |
| orbit number at epoch: | 4470 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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