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 26022.46714128 +.00000000 +00000-0 +18991-3 0 00004
2 16864 74.0279 38.3393 0030577 86.2090 274.2562 14.42232137 09
| Epoch (UTC): | 22 January 2026 11:12:41 |
| Eccentricity: | 0.0030577 |
| inclination: | 74.0279° |
| perigee height: | 729 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 38.3393° |
| argument of perigee: | 86.2090° |
| revolutions per day: | 14.42232137 |
| mean anomaly at epoch: | 274.2562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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