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 49264U 26145.10745370 +.00000000 +00000-0 +28768-3 0 00007
2 49264 97.3883 206.5755 0013496 141.1057 219.1155 15.25613316 04
| Epoch (UTC): | 25 May 2026 02:34:44 |
| Eccentricity: | 0.0013496 |
| inclination: | 97.3883° |
| perigee height: | 480 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 206.5755° |
| argument of perigee: | 141.1057° |
| revolutions per day: | 15.25613316 |
| mean anomaly at epoch: | 219.1155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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