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 46160U 26145.04783963 +.00000000 +00000-0 +69898-3 0 00001
2 46160 53.0454 271.1701 0002917 156.1690 203.9461 15.69309083 05
| Epoch (UTC): | 25 May 2026 01:08:53 |
| Eccentricity: | 0.0002917 |
| inclination: | 53.0454° |
| perigee height: | 359 km |
| apogee height: | 363 km |
| right ascension of ascending node: | 271.1701° |
| argument of perigee: | 156.1690° |
| revolutions per day: | 15.69309083 |
| mean anomaly at epoch: | 203.9461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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