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 36122U 26102.12464660 +.00000000 +00000-0 -65950-4 0 00007
2 36122 100.3968 57.0302 0007927 28.8168 331.3381 13.16437771 00
| Epoch (UTC): | 12 April 2026 02:59:29 |
| Eccentricity: | 0.0007927 |
| inclination: | 100.3968° |
| perigee height: | 1192 km |
| apogee height: | 1204 km |
| right ascension of ascending node: | 57.0302° |
| argument of perigee: | 28.8168° |
| revolutions per day: | 13.16437771 |
| mean anomaly at epoch: | 331.3381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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