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 46353U 26145.55851977 +.00000000 +00000-0 +75761-3 0 00008
2 46353 53.0427 345.2414 0005139 132.6179 227.5270 15.66333272 07
| Epoch (UTC): | 25 May 2026 13:24:16 |
| Eccentricity: | 0.0005139 |
| inclination: | 53.0427° |
| perigee height: | 366 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 345.2414° |
| argument of perigee: | 132.6179° |
| revolutions per day: | 15.66333272 |
| mean anomaly at epoch: | 227.5270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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