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 63804U 26145.34799529 +.00000000 +00000-0 +62088-3 0 00007
2 63804 43.0016 100.0481 0001579 257.2554 102.8121 15.27589773 02
| Epoch (UTC): | 25 May 2026 08:21:06 |
| Eccentricity: | 0.0001579 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.0481° |
| argument of perigee: | 257.2554° |
| revolutions per day: | 15.27589773 |
| mean anomaly at epoch: | 102.8121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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