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 64280U 26145.36940516 +.00000000 +00000-0 +52413-3 0 00003
2 64280 53.1570 120.6952 0000759 75.8442 284.2643 15.30211066 03
| Epoch (UTC): | 25 May 2026 08:51:56 |
| Eccentricity: | 0.0000759 |
| inclination: | 53.1570° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.6952° |
| argument of perigee: | 75.8442° |
| revolutions per day: | 15.30211066 |
| mean anomaly at epoch: | 284.2643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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