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 64884U 26145.58799698 +.00000000 +00000-0 +33343-3 0 00001
2 64884 97.4551 114.0218 0005244 246.4721 113.5969 15.29082729 00
| Epoch (UTC): | 25 May 2026 14:06:42 |
| Eccentricity: | 0.0005244 |
| inclination: | 97.4551° |
| perigee height: | 475 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 114.0218° |
| argument of perigee: | 246.4721° |
| revolutions per day: | 15.29082729 |
| mean anomaly at epoch: | 113.5969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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