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 16182U 85097B 25189.04912510 -.00000217 00000-0 -84892-4 0 9991
2 16182 71.0039 295.5705 0009834 270.0313 262.4362 14.16556052 52897
| Epoch (UTC): | 08 July 2025 01:10:44 |
| Eccentricity: | 0.0009834 |
| inclination: | 71.0039° |
| perigee height: | 830 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 295.5705° |
| argument of perigee: | 270.0313° |
| revolutions per day: | 14.16556052 |
| mean anomaly at epoch: | 262.4362° |
| orbit number at epoch: | 5289 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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