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 64182U 26145.55262759 +.00000000 +00000-0 +81074-3 0 00006
2 64182 53.1562 94.0726 0001287 84.5635 275.5513 15.30205357 01
| Epoch (UTC): | 25 May 2026 13:15:47 |
| Eccentricity: | 0.0001287 |
| inclination: | 53.1562° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 94.0726° |
| argument of perigee: | 84.5635° |
| revolutions per day: | 15.30205357 |
| mean anomaly at epoch: | 275.5513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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