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 65373U 26145.33452565 +.00000000 +00000-0 +58669-3 0 00005
2 65373 53.1593 171.8957 0000896 49.0780 311.0301 15.34399006 00
| Epoch (UTC): | 25 May 2026 08:01:43 |
| Eccentricity: | 0.0000896 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 171.8957° |
| argument of perigee: | 49.0780° |
| revolutions per day: | 15.34399006 |
| mean anomaly at epoch: | 311.0301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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