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 64381U 26145.56358756 +.00000000 +00000-0 +21808-2 0 00009
2 64381 42.9982 341.0709 0002561 272.9002 87.1572 15.70919383 04
| Epoch (UTC): | 25 May 2026 13:31:33 |
| Eccentricity: | 0.0002561 |
| inclination: | 42.9982° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 341.0709° |
| argument of perigee: | 272.9002° |
| revolutions per day: | 15.70919383 |
| mean anomaly at epoch: | 87.1572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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