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 63885U 26145.12839339 +.00000000 +00000-0 +33224-3 0 00006
2 63885 70.0022 41.7001 0002712 270.9237 89.1612 14.98338817 07
| Epoch (UTC): | 25 May 2026 03:04:53 |
| Eccentricity: | 0.0002712 |
| inclination: | 70.0022° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.7001° |
| argument of perigee: | 270.9237° |
| revolutions per day: | 14.98338817 |
| mean anomaly at epoch: | 89.1612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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