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 64894U 26145.61458990 +.00000000 +00000-0 +80115-3 0 00002
2 64894 97.4477 116.6011 0001886 237.9162 122.1902 15.42036150 04
| Epoch (UTC): | 25 May 2026 14:45:00 |
| Eccentricity: | 0.0001886 |
| inclination: | 97.4477° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 116.6011° |
| argument of perigee: | 237.9162° |
| revolutions per day: | 15.42036150 |
| mean anomaly at epoch: | 122.1902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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