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 64424U 26145.53979654 +.00000000 +00000-0 +19947-3 0 00002
2 64424 70.0010 240.8896 0003250 263.6577 96.4212 14.98338888 07
| Epoch (UTC): | 25 May 2026 12:57:18 |
| Eccentricity: | 0.0003250 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 240.8896° |
| argument of perigee: | 263.6577° |
| revolutions per day: | 14.98338888 |
| mean anomaly at epoch: | 96.4212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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