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 22827U 26142.13735617 +.00000000 +00000-0 +56685-4 0 00006
2 22827 98.6417 210.6433 0010035 103.2267 315.8823 14.32535888 04
| Epoch (UTC): | 22 May 2026 03:17:47 |
| Eccentricity: | 0.0010035 |
| inclination: | 98.6417° |
| perigee height: | 776 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 210.6433° |
| argument of perigee: | 103.2267° |
| revolutions per day: | 14.32535888 |
| mean anomaly at epoch: | 315.8823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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