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 46743U 26145.36265902 +.00000000 +00000-0 +84053-3 0 00001
2 46743 53.0403 280.7770 0006101 293.2883 66.7489 15.65948988 08
| Epoch (UTC): | 25 May 2026 08:42:13 |
| Eccentricity: | 0.0006101 |
| inclination: | 53.0403° |
| perigee height: | 366 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 280.7770° |
| argument of perigee: | 293.2883° |
| revolutions per day: | 15.65948988 |
| mean anomaly at epoch: | 66.7489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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