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 25188.01628112 .00015316 00000-0 29875-3 0 9991
2 16326 82.4940 171.6753 0007588 121.4011 238.7982 15.47336826163638
| Epoch (UTC): | 07 July 2025 00:23:26 |
| Eccentricity: | 0.0007588 |
| inclination: | 82.4940° |
| perigee height: | 419 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 171.6753° |
| argument of perigee: | 121.4011° |
| revolutions per day: | 15.47336826 |
| mean anomaly at epoch: | 238.7982° |
| orbit number at epoch: | 16363 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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