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 64700U 26145.37969990 +.00000000 +00000-0 +35868-3 0 00003
2 64700 70.0002 121.2471 0003982 265.9741 94.0963 14.98335639 04
| Epoch (UTC): | 25 May 2026 09:06:46 |
| Eccentricity: | 0.0003982 |
| inclination: | 70.0002° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.2471° |
| argument of perigee: | 265.9741° |
| revolutions per day: | 14.98335639 |
| mean anomaly at epoch: | 94.0963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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