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 64906U 26145.30099843 +.00000000 +00000-0 +55919-3 0 00004
2 64906 53.1616 349.7960 0001060 81.6878 278.4243 15.30215705 01
| Epoch (UTC): | 25 May 2026 07:13:26 |
| Eccentricity: | 0.0001060 |
| inclination: | 53.1616° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 349.7960° |
| argument of perigee: | 81.6878° |
| revolutions per day: | 15.30215705 |
| mean anomaly at epoch: | 278.4243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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