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 42794U 26153.38766676 +.00000000 +00000-0 +24218-3 0 00005
2 42794 97.5551 132.3457 0080967 211.8768 147.7552 15.16873350 08
| Epoch (UTC): | 02 June 2026 09:18:14 |
| Eccentricity: | 0.0080967 |
| inclination: | 97.5551° |
| perigee height: | 459 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 132.3457° |
| argument of perigee: | 211.8768° |
| revolutions per day: | 15.16873350 |
| mean anomaly at epoch: | 147.7552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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