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 64733U 26145.47326502 +.00000000 +00000-0 +23977-3 0 00004
2 64733 53.1583 181.1367 0001114 85.8096 274.3034 15.34392809 07
| Epoch (UTC): | 25 May 2026 11:21:30 |
| Eccentricity: | 0.0001114 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 181.1367° |
| argument of perigee: | 85.8096° |
| revolutions per day: | 15.34392809 |
| mean anomaly at epoch: | 274.3034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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