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 51734U 26145.49060579 +.00000000 +00000-0 +92343-4 0 00006
2 51734 53.2138 334.3509 0001374 105.6564 254.4580 15.08841161 06
| Epoch (UTC): | 25 May 2026 11:46:28 |
| Eccentricity: | 0.0001374 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.3509° |
| argument of perigee: | 105.6564° |
| revolutions per day: | 15.08841161 |
| mean anomaly at epoch: | 254.4580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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