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 64037U 26145.34413909 +.00000000 +00000-0 +26907-3 0 00001
2 64037 70.0005 281.1977 0002484 272.6192 87.4682 14.98338152 05
| Epoch (UTC): | 25 May 2026 08:15:33 |
| Eccentricity: | 0.0002484 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.1977° |
| argument of perigee: | 272.6192° |
| revolutions per day: | 14.98338152 |
| mean anomaly at epoch: | 87.4682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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