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 is defined by the following mean orbital elements,
1 16615U 26100.04572167 +.00000000 +00000-0 +98161-4 0 00002
2 16615 98.2205 116.1002 0010743 220.1897 198.6968 14.33313115 04
| Epoch (UTC): | 10 April 2026 01:05:50 |
| Eccentricity: | 0.0010743 |
| inclination: | 98.2205° |
| perigee height: | 773 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 116.1002° |
| argument of perigee: | 220.1897° |
| revolutions per day: | 14.33313115 |
| mean anomaly at epoch: | 198.6968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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