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 26050.42746115 +.00000000 +00000-0 +34197-3 0 00009
2 42794 97.5458 29.8873 0083552 208.4647 151.2009 15.15210623 01
| Epoch (UTC): | 19 February 2026 10:15:32 |
| Eccentricity: | 0.0083552 |
| inclination: | 97.5458° |
| perigee height: | 463 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 29.8873° |
| argument of perigee: | 208.4647° |
| revolutions per day: | 15.15210623 |
| mean anomaly at epoch: | 151.2009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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