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 46396U 26145.60308876 +.00000000 +00000-0 +22180-3 0 00003
2 46396 97.5108 271.5972 0018101 24.1391 336.0690 15.23331881 06
| Epoch (UTC): | 25 May 2026 14:28:26 |
| Eccentricity: | 0.0018101 |
| inclination: | 97.5108° |
| perigee height: | 483 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 271.5972° |
| argument of perigee: | 24.1391° |
| revolutions per day: | 15.23331881 |
| mean anomaly at epoch: | 336.0690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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