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 38012U 26145.64482480 +.00000000 +00000-0 +11593-3 0 00003
2 38012 98.1974 221.0495 0001280 104.9664 63.8257 14.58554746 08
| Epoch (UTC): | 25 May 2026 15:28:32 |
| Eccentricity: | 0.0001280 |
| inclination: | 98.1974° |
| perigee height: | 697 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 221.0495° |
| argument of perigee: | 104.9664° |
| revolutions per day: | 14.58554746 |
| mean anomaly at epoch: | 63.8257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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