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 64380U 26145.57951946 +.00000000 +00000-0 +16709-2 0 00003
2 64380 42.9995 341.2015 0001941 259.6333 100.4316 15.70891278 06
| Epoch (UTC): | 25 May 2026 13:54:30 |
| Eccentricity: | 0.0001941 |
| inclination: | 42.9995° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 341.2015° |
| argument of perigee: | 259.6333° |
| revolutions per day: | 15.70891278 |
| mean anomaly at epoch: | 100.4316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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