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 64245U 26144.26642368 +.00000000 +00000-0 +12310-2 0 00007
2 64245 43.0022 113.3199 0001533 266.5078 93.5614 15.70847868 09
| Epoch (UTC): | 24 May 2026 06:23:39 |
| Eccentricity: | 0.0001533 |
| inclination: | 43.0022° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 113.3199° |
| argument of perigee: | 266.5078° |
| revolutions per day: | 15.70847868 |
| mean anomaly at epoch: | 93.5614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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