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 64307U 26145.58335647 +.00000000 +00000-0 +20561-2 0 00008
2 64307 70.0022 0.7390 0002418 263.9006 53.5823 14.98325937 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002418 |
| inclination: | 70.0022° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 0.7390° |
| argument of perigee: | 263.9006° |
| revolutions per day: | 14.98325937 |
| mean anomaly at epoch: | 53.5823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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