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 63930U 26145.23318134 +.00000000 +00000-0 +28380-3 0 00001
2 63930 70.0007 81.6395 0003040 269.0203 91.0608 14.98338801 07
| Epoch (UTC): | 25 May 2026 05:35:46 |
| Eccentricity: | 0.0003040 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.6395° |
| argument of perigee: | 269.0203° |
| revolutions per day: | 14.98338801 |
| mean anomaly at epoch: | 91.0608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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