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 64677U 26145.31563017 +.00000000 +00000-0 +51096-3 0 00001
2 64677 53.1593 120.6361 0001093 79.4394 280.6730 15.30208906 06
| Epoch (UTC): | 25 May 2026 07:34:30 |
| Eccentricity: | 0.0001093 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.6361° |
| argument of perigee: | 79.4394° |
| revolutions per day: | 15.30208906 |
| mean anomaly at epoch: | 280.6730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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