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 26020.52492030 +.00000000 +00000-0 +14572-3 0 00005
2 16864 74.0279 41.9431 0030570 90.4765 269.9894 14.42228939 05
| Epoch (UTC): | 20 January 2026 12:35:53 |
| Eccentricity: | 0.0030570 |
| inclination: | 74.0279° |
| perigee height: | 729 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 41.9431° |
| argument of perigee: | 90.4765° |
| revolutions per day: | 14.42228939 |
| mean anomaly at epoch: | 269.9894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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