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 42349U 26086.38944286 +.00000000 +00000-0 +12669-2 0 00007
2 42349 98.6674 147.5807 0006286 347.4103 12.6918 14.24862846 02
| Epoch (UTC): | 27 March 2026 09:20:47 |
| Eccentricity: | 0.0006286 |
| inclination: | 98.6674° |
| perigee height: | 804 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 147.5807° |
| argument of perigee: | 347.4103° |
| revolutions per day: | 14.24862846 |
| mean anomaly at epoch: | 12.6918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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