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 64883U 26145.58807398 +.00000000 +00000-0 +30678-3 0 00005
2 64883 97.4558 114.0283 0005260 250.2970 109.7702 15.29126004 02
| Epoch (UTC): | 25 May 2026 14:06:49 |
| Eccentricity: | 0.0005260 |
| inclination: | 97.4558° |
| perigee height: | 475 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 114.0283° |
| argument of perigee: | 250.2970° |
| revolutions per day: | 15.29126004 |
| mean anomaly at epoch: | 109.7702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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