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 26073.58814481 +.00000000 +00000-0 +85940-4 0 00005
2 16864 74.0284 303.4937 0032289 337.3417 22.6311 14.42277838 04
| Epoch (UTC): | 14 March 2026 14:06:55 |
| Eccentricity: | 0.0032289 |
| inclination: | 74.0284° |
| perigee height: | 728 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 303.4937° |
| argument of perigee: | 337.3417° |
| revolutions per day: | 14.42277838 |
| mean anomaly at epoch: | 22.6311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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