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 64412U 26145.53128036 +.00000000 +00000-0 +23691-3 0 00000
2 64412 70.0007 240.8523 0003550 269.1494 90.9258 14.98335408 03
| Epoch (UTC): | 25 May 2026 12:45:02 |
| Eccentricity: | 0.0003550 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 240.8523° |
| argument of perigee: | 269.1494° |
| revolutions per day: | 14.98335408 |
| mean anomaly at epoch: | 90.9258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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