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 22826U 26038.16757285 +.00000000 +00000-0 +92806-4 0 00002
2 22826 98.6996 105.4489 0010007 104.6222 255.6071 14.31325887 03
| Epoch (UTC): | 07 February 2026 04:01:18 |
| Eccentricity: | 0.0010007 |
| inclination: | 98.6996° |
| perigee height: | 780 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 105.4489° |
| argument of perigee: | 104.6222° |
| revolutions per day: | 14.31325887 |
| mean anomaly at epoch: | 255.6071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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