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 48465U 26145.48519113 +.00000000 +00000-0 +49350-3 0 00004
2 48465 53.1397 185.8316 0002774 18.7817 341.3296 15.53081444 04
| Epoch (UTC): | 25 May 2026 11:38:40 |
| Eccentricity: | 0.0002774 |
| inclination: | 53.1397° |
| perigee height: | 406 km |
| apogee height: | 410 km |
| right ascension of ascending node: | 185.8316° |
| argument of perigee: | 18.7817° |
| revolutions per day: | 15.53081444 |
| mean anomaly at epoch: | 341.3296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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