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 63790U 26145.57437535 +.00000000 +00000-0 +41650-3 0 00004
2 63790 43.0023 338.0653 0001519 265.2943 94.7735 15.27589514 06
| Epoch (UTC): | 25 May 2026 13:47:06 |
| Eccentricity: | 0.0001519 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.0653° |
| argument of perigee: | 265.2943° |
| revolutions per day: | 15.27589514 |
| mean anomaly at epoch: | 94.7735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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