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 26074.07368330 +.00000000 +00000-0 +81294-4 0 00005
2 16864 74.0283 302.5927 0032305 336.3325 23.6343 14.42278000 06
| Epoch (UTC): | 15 March 2026 01:46:06 |
| Eccentricity: | 0.0032305 |
| inclination: | 74.0283° |
| perigee height: | 728 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 302.5927° |
| argument of perigee: | 336.3325° |
| revolutions per day: | 14.42278000 |
| mean anomaly at epoch: | 23.6343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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