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 64392U 26145.32527157 +.00000000 +00000-0 +58788-3 0 00006
2 64392 42.9996 107.3185 0001148 270.2011 89.8709 15.27586249 07
| Epoch (UTC): | 25 May 2026 07:48:23 |
| Eccentricity: | 0.0001148 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.3185° |
| argument of perigee: | 270.2011° |
| revolutions per day: | 15.27586249 |
| mean anomaly at epoch: | 89.8709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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