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 64606U 26145.53906477 +.00000000 +00000-0 +11116-2 0 00006
2 64606 53.1600 338.0794 0001184 64.1498 295.9624 15.30214101 04
| Epoch (UTC): | 25 May 2026 12:56:15 |
| Eccentricity: | 0.0001184 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.0794° |
| argument of perigee: | 64.1498° |
| revolutions per day: | 15.30214101 |
| mean anomaly at epoch: | 295.9624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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