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 64415U 26145.51875953 +.00000000 +00000-0 +18897-3 0 00000
2 64415 70.0007 240.8191 0003355 268.6149 91.4626 14.98333254 03
| Epoch (UTC): | 25 May 2026 12:27:00 |
| Eccentricity: | 0.0003355 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 240.8191° |
| argument of perigee: | 268.6149° |
| revolutions per day: | 14.98333254 |
| mean anomaly at epoch: | 91.4626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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