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 46352U 26145.57226575 +.00000000 +00000-0 +75986-3 0 00008
2 46352 53.0386 303.9349 0007071 168.3009 191.8175 15.73714840 02
| Epoch (UTC): | 25 May 2026 13:44:03 |
| Eccentricity: | 0.0007071 |
| inclination: | 53.0386° |
| perigee height: | 344 km |
| apogee height: | 353 km |
| right ascension of ascending node: | 303.9349° |
| argument of perigee: | 168.3009° |
| revolutions per day: | 15.73714840 |
| mean anomaly at epoch: | 191.8175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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