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 26150.84008352 +.00000000 +00000-0 +96618-3 0 00004
2 36122 100.4015 104.9501 0006813 275.0753 84.9582 13.16440060 05
| Epoch (UTC): | 30 May 2026 20:09:43 |
| Eccentricity: | 0.0006813 |
| inclination: | 100.4015° |
| perigee height: | 1193 km |
| apogee height: | 1204 km |
| right ascension of ascending node: | 104.9501° |
| argument of perigee: | 275.0753° |
| revolutions per day: | 13.16440060 |
| mean anomaly at epoch: | 84.9582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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