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 41784U 26150.43377279 +.00000000 +00000-0 +20666-3 0 00006
2 41784 97.8178 151.6501 0027482 261.9226 97.8862 14.68949055 07
| Epoch (UTC): | 30 May 2026 10:24:37 |
| Eccentricity: | 0.0027482 |
| inclination: | 97.8178° |
| perigee height: | 645 km |
| apogee height: | 684 km |
| right ascension of ascending node: | 151.6501° |
| argument of perigee: | 261.9226° |
| revolutions per day: | 14.68949055 |
| mean anomaly at epoch: | 97.8862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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