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 46384U 26145.58335647 +.00000000 +00000-0 +31850-4 0 00008
2 46384 53.0382 335.7668 0000914 85.1894 137.1869 15.61201946 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000914 |
| inclination: | 53.0382° |
| perigee height: | 384 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 335.7668° |
| argument of perigee: | 85.1894° |
| revolutions per day: | 15.61201946 |
| mean anomaly at epoch: | 137.1869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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