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 63927U 26145.33335647 +.00000000 +00000-0 +35299-3 0 00003
2 63927 70.0006 81.0542 0003105 278.2561 194.5909 14.98348768 07
| Epoch (UTC): | 25 May 2026 08:00:01 |
| Eccentricity: | 0.0003105 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.0542° |
| argument of perigee: | 278.2561° |
| revolutions per day: | 14.98348768 |
| mean anomaly at epoch: | 194.5909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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