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 64436U 26145.52309615 +.00000000 +00000-0 +22580-3 0 00005
2 64436 70.0008 240.8200 0003089 269.1070 90.9735 14.98336870 03
| Epoch (UTC): | 25 May 2026 12:33:15 |
| Eccentricity: | 0.0003089 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 240.8200° |
| argument of perigee: | 269.1070° |
| revolutions per day: | 14.98336870 |
| mean anomaly at epoch: | 90.9735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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