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 64433U 26145.53144539 +.00000000 +00000-0 +21594-3 0 00009
2 64433 70.0004 240.8563 0003560 268.3200 91.7552 14.98335484 04
| Epoch (UTC): | 25 May 2026 12:45:16 |
| Eccentricity: | 0.0003560 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 240.8563° |
| argument of perigee: | 268.3200° |
| revolutions per day: | 14.98335484 |
| mean anomaly at epoch: | 91.7552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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