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 16326U 85113A 25196.93983930 .00017541 00000-0 33874-3 0 9999
2 16326 82.4958 162.4228 0007876 98.9973 261.2169 15.47626688165017
| Epoch (UTC): | 15 July 2025 22:33:22 |
| Eccentricity: | 0.0007876 |
| inclination: | 82.4958° |
| perigee height: | 418 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 162.4228° |
| argument of perigee: | 98.9973° |
| revolutions per day: | 15.47626688 |
| mean anomaly at epoch: | 261.2169° |
| orbit number at epoch: | 16501 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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