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 26066.16633161 +.00000000 +00000-0 +10611-3 0 00007
2 16864 74.0296 317.2640 0032008 352.7036 7.3650 14.42272847 09
| Epoch (UTC): | 07 March 2026 03:59:31 |
| Eccentricity: | 0.0032008 |
| inclination: | 74.0296° |
| perigee height: | 728 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 317.2640° |
| argument of perigee: | 352.7036° |
| revolutions per day: | 14.42272847 |
| mean anomaly at epoch: | 7.3650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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