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 49258U 26142.98125317 +.00000000 +00000-0 +00000-0 0 00002
2 49258 63.1042 222.9236 6937178 269.8776 17.5667 2.00634461 06
| Epoch (UTC): | 22 May 2026 23:33:00 |
| Eccentricity: | 0.6937178 |
| inclination: | 63.1042° |
| perigee height: | 1755 km |
| apogee height: | 38597 km |
| right ascension of ascending node: | 222.9236° |
| argument of perigee: | 269.8776° |
| revolutions per day: | 2.00634461 |
| mean anomaly at epoch: | 17.5667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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