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 46073U 26145.33742161 +.00000000 +00000-0 +40747-5 0 00005
2 46073 53.1621 108.2415 0001252 93.0013 267.1132 15.31702579 09
| Epoch (UTC): | 25 May 2026 08:05:53 |
| Eccentricity: | 0.0001252 |
| inclination: | 53.1621° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 108.2415° |
| argument of perigee: | 93.0013° |
| revolutions per day: | 15.31702579 |
| mean anomaly at epoch: | 267.1132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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