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 63846U 26145.31349564 +.00000000 +00000-0 +88491-3 0 00006
2 63846 43.0034 4.9259 0000979 269.6293 90.4447 15.27589393 04
| Epoch (UTC): | 25 May 2026 07:31:26 |
| Eccentricity: | 0.0000979 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 4.9259° |
| argument of perigee: | 269.6293° |
| revolutions per day: | 15.27589393 |
| mean anomaly at epoch: | 90.4447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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