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 64270U 26145.24827566 +.00000000 +00000-0 +25917-3 0 00007
2 64270 53.1601 121.3604 0001206 108.6635 251.4497 15.30200871 01
| Epoch (UTC): | 25 May 2026 05:57:31 |
| Eccentricity: | 0.0001206 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 121.3604° |
| argument of perigee: | 108.6635° |
| revolutions per day: | 15.30200871 |
| mean anomaly at epoch: | 251.4497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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