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 41783U 26145.46512647 +.00000000 +00000-0 +11677-3 0 00004
2 41783 97.8321 143.3221 0029823 292.1929 67.6113 14.67160519 03
| Epoch (UTC): | 25 May 2026 11:09:46 |
| Eccentricity: | 0.0029823 |
| inclination: | 97.8321° |
| perigee height: | 649 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 143.3221° |
| argument of perigee: | 292.1929° |
| revolutions per day: | 14.67160519 |
| mean anomaly at epoch: | 67.6113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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