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 63869U 26145.12021068 +.00000000 +00000-0 +31323-3 0 00008
2 63869 70.0019 41.6732 0002624 269.5826 90.5032 14.98338483 06
| Epoch (UTC): | 25 May 2026 02:53:06 |
| Eccentricity: | 0.0002624 |
| inclination: | 70.0019° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.6732° |
| argument of perigee: | 269.5826° |
| revolutions per day: | 14.98338483 |
| mean anomaly at epoch: | 90.5032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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