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 51469U 26145.66724686 +.00000000 +00000-0 +36965-4 0 00004
2 51469 53.2126 293.5549 0001238 89.6292 270.4842 15.08843095 03
| Epoch (UTC): | 25 May 2026 16:00:50 |
| Eccentricity: | 0.0001238 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 293.5549° |
| argument of perigee: | 89.6292° |
| revolutions per day: | 15.08843095 |
| mean anomaly at epoch: | 270.4842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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