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 64038U 26145.51503706 +.00000000 +00000-0 +15498-3 0 00009
2 64038 69.9998 280.5924 0003364 262.7535 97.3242 14.98331720 04
| Epoch (UTC): | 25 May 2026 12:21:39 |
| Eccentricity: | 0.0003364 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 280.5924° |
| argument of perigee: | 262.7535° |
| revolutions per day: | 14.98331720 |
| mean anomaly at epoch: | 97.3242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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