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 25198.87951116 .00019109 00000-0 36809-3 0 9998
2 16326 82.4955 160.4110 0007880 94.3072 265.9079 15.47700896165315
| Epoch (UTC): | 17 July 2025 21:06:29 |
| Eccentricity: | 0.0007880 |
| inclination: | 82.4955° |
| perigee height: | 418 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 160.4110° |
| argument of perigee: | 94.3072° |
| revolutions per day: | 15.47700896 |
| mean anomaly at epoch: | 265.9079° |
| orbit number at epoch: | 16531 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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