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 64212U 26145.00145628 +.00000000 +00000-0 +49098-3 0 00005
2 64212 53.1589 44.8407 0001266 68.0008 292.1127 15.30196047 02
| Epoch (UTC): | 25 May 2026 00:02:05 |
| Eccentricity: | 0.0001266 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.8407° |
| argument of perigee: | 68.0008° |
| revolutions per day: | 15.30196047 |
| mean anomaly at epoch: | 292.1127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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