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 64477U 26145.31508044 +.00000000 +00000-0 +85511-3 0 00007
2 64477 53.1594 118.5040 0001299 81.0878 279.0272 15.35410208 07
| Epoch (UTC): | 25 May 2026 07:33:42 |
| Eccentricity: | 0.0001299 |
| inclination: | 53.1594° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 118.5040° |
| argument of perigee: | 81.0878° |
| revolutions per day: | 15.35410208 |
| mean anomaly at epoch: | 279.0272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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