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 51814U 26145.53385228 +.00000000 +00000-0 +38950-4 0 00005
2 51814 53.2135 344.1543 0001343 90.5318 269.5828 15.08836146 03
| Epoch (UTC): | 25 May 2026 12:48:44 |
| Eccentricity: | 0.0001343 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 344.1543° |
| argument of perigee: | 90.5318° |
| revolutions per day: | 15.08836146 |
| mean anomaly at epoch: | 269.5828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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