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 64463U 26145.15019664 +.00000000 +00000-0 +17068-2 0 00000
2 64463 53.1578 95.9252 0001346 85.6190 274.4965 15.30248750 01
| Epoch (UTC): | 25 May 2026 03:36:16 |
| Eccentricity: | 0.0001346 |
| inclination: | 53.1578° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.9252° |
| argument of perigee: | 85.6190° |
| revolutions per day: | 15.30248750 |
| mean anomaly at epoch: | 274.4965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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