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 64152U 26145.61935029 +.00000000 +00000-0 +53773-3 0 00002
2 64152 97.4454 196.9631 0001389 138.0593 222.0741 15.05662954 09
| Epoch (UTC): | 25 May 2026 14:51:51 |
| Eccentricity: | 0.0001389 |
| inclination: | 97.4454° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 196.9631° |
| argument of perigee: | 138.0593° |
| revolutions per day: | 15.05662954 |
| mean anomaly at epoch: | 222.0741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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