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 63858U 26145.65841029 +.00000000 +00000-0 +81590-3 0 00002
2 63858 43.0033 3.1816 0001174 245.7288 114.3442 15.27585182 06
| Epoch (UTC): | 25 May 2026 15:48:06 |
| Eccentricity: | 0.0001174 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.1816° |
| argument of perigee: | 245.7288° |
| revolutions per day: | 15.27585182 |
| mean anomaly at epoch: | 114.3442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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