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 64703U 26145.38816677 +.00000000 +00000-0 +21827-3 0 00000
2 64703 70.0000 120.8785 0003467 269.5051 90.5711 14.98335910 04
| Epoch (UTC): | 25 May 2026 09:18:57 |
| Eccentricity: | 0.0003467 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 120.8785° |
| argument of perigee: | 269.5051° |
| revolutions per day: | 14.98335910 |
| mean anomaly at epoch: | 90.5711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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