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 51651U 26145.43109186 +.00000000 +00000-0 -18741-2 0 00005
2 51651 87.8853 40.8114 0001890 71.4381 288.6951 13.10373699 00
| Epoch (UTC): | 25 May 2026 10:20:46 |
| Eccentricity: | 0.0001890 |
| inclination: | 87.8853° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8114° |
| argument of perigee: | 71.4381° |
| revolutions per day: | 13.10373699 |
| mean anomaly at epoch: | 288.6951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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