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 16864U 26071.09108858 +.00000000 +00000-0 +83642-4 0 00000
2 16864 74.0289 308.1268 0032206 342.4753 17.5289 14.42276225 03
| Epoch (UTC): | 12 March 2026 02:11:10 |
| Eccentricity: | 0.0032206 |
| inclination: | 74.0289° |
| perigee height: | 728 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 308.1268° |
| argument of perigee: | 342.4753° |
| revolutions per day: | 14.42276225 |
| mean anomaly at epoch: | 17.5289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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