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 20122U 26150.47134692 +.00000000 +00000-0 +00000-0 0 00000
2 20122 12.2606 334.0689 0013775 357.7904 219.6175 1.01366540 04
| Epoch (UTC): | 30 May 2026 11:18:44 |
| Eccentricity: | 0.0013775 |
| inclination: | 12.2606° |
| perigee height: | 35425 km |
| apogee height: | 35540 km |
| right ascension of ascending node: | 334.0689° |
| argument of perigee: | 357.7904° |
| revolutions per day: | 1.01366540 |
| mean anomaly at epoch: | 219.6175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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