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 16615U 86019C 25189.06980694 .00000174 00000-0 78379-4 0 9990
2 16615 98.2369 213.7572 0010930 334.8042 83.2574 14.33093168 60689
| Epoch (UTC): | 08 July 2025 01:40:31 |
| Eccentricity: | 0.0010930 |
| inclination: | 98.2369° |
| perigee height: | 773 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 213.7572° |
| argument of perigee: | 334.8042° |
| revolutions per day: | 14.33093168 |
| mean anomaly at epoch: | 83.2574° |
| orbit number at epoch: | 6068 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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