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 63859U 26144.95328000 +.00000000 +00000-0 +15557-2 0 00003
2 63859 43.0021 7.3382 0001446 280.1706 79.8982 15.27638928 09
| Epoch (UTC): | 24 May 2026 22:52:43 |
| Eccentricity: | 0.0001446 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 7.3382° |
| argument of perigee: | 280.1706° |
| revolutions per day: | 15.27638928 |
| mean anomaly at epoch: | 79.8982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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