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 22816U 26017.58588670 +.00000000 +00000-0 +44887-2 0 00008
2 22816 71.4437 87.3260 0051602 243.3418 116.2450 14.74223519 09
| Epoch (UTC): | 17 January 2026 14:03:40 |
| Eccentricity: | 0.0051602 |
| inclination: | 71.4437° |
| perigee height: | 611 km |
| apogee height: | 684 km |
| right ascension of ascending node: | 87.3260° |
| argument of perigee: | 243.3418° |
| revolutions per day: | 14.74223519 |
| mean anomaly at epoch: | 116.2450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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