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 64481U 26145.25136977 +.00000000 +00000-0 +67788-3 0 00003
2 64481 53.1605 120.9412 0001082 123.9575 236.1529 15.30210339 02
| Epoch (UTC): | 25 May 2026 06:01:58 |
| Eccentricity: | 0.0001082 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.9412° |
| argument of perigee: | 123.9575° |
| revolutions per day: | 15.30210339 |
| mean anomaly at epoch: | 236.1529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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