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 42070U 26144.99163681 +.00000000 +00000-0 +00000-0 0 00006
2 42070 0.0182 307.9842 0002094 120.8535 60.8345 1.00272052 03
| Epoch (UTC): | 24 May 2026 23:47:57 |
| Eccentricity: | 0.0002094 |
| inclination: | 0.0182° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 307.9842° |
| argument of perigee: | 120.8535° |
| revolutions per day: | 1.00272052 |
| mean anomaly at epoch: | 60.8345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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