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 42831U 26150.58718206 +.00000000 +00000-0 +32936-3 0 00008
2 42831 97.4607 306.8068 0018623 180.0674 180.0551 15.01017055 05
| Epoch (UTC): | 30 May 2026 14:05:32 |
| Eccentricity: | 0.0018623 |
| inclination: | 97.4607° |
| perigee height: | 551 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 306.8068° |
| argument of perigee: | 180.0674° |
| revolutions per day: | 15.01017055 |
| mean anomaly at epoch: | 180.0551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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