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 64062U 26145.26045905 +.00000000 +00000-0 +00000-0 0 00000
2 64062 0.0446 98.7450 0002283 359.4386 45.7568 1.00272284 01
| Epoch (UTC): | 25 May 2026 06:15:03 |
| Eccentricity: | 0.0002283 |
| inclination: | 0.0446° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 98.7450° |
| argument of perigee: | 359.4386° |
| revolutions per day: | 1.00272284 |
| mean anomaly at epoch: | 45.7568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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