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 25198.36227429 .00019981 00000-0 38513-3 0 9997
2 16326 82.4955 160.9475 0007880 95.6041 264.6108 15.47682270165239
| Epoch (UTC): | 17 July 2025 08:41:40 |
| Eccentricity: | 0.0007880 |
| inclination: | 82.4955° |
| perigee height: | 418 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 160.9475° |
| argument of perigee: | 95.6041° |
| revolutions per day: | 15.47682270 |
| mean anomaly at epoch: | 264.6108° |
| orbit number at epoch: | 16523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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