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 51464U 26145.66356757 +.00000000 +00000-0 +65433-4 0 00001
2 51464 53.2141 293.5727 0001374 90.2502 269.8648 15.08840386 02
| Epoch (UTC): | 25 May 2026 15:55:32 |
| Eccentricity: | 0.0001374 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 293.5727° |
| argument of perigee: | 90.2502° |
| revolutions per day: | 15.08840386 |
| mean anomaly at epoch: | 269.8648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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