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 49256U 26145.57074222 +.00000000 +00000-0 +25679-3 0 00008
2 49256 97.6443 268.3239 0032690 220.0380 139.8439 15.10398426 05
| Epoch (UTC): | 25 May 2026 13:41:52 |
| Eccentricity: | 0.0032690 |
| inclination: | 97.6443° |
| perigee height: | 512 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 268.3239° |
| argument of perigee: | 220.0380° |
| revolutions per day: | 15.10398426 |
| mean anomaly at epoch: | 139.8439° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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