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 51646U 26145.66516106 +.00000000 +00000-0 -14794-2 0 00002
2 51646 87.8865 40.7347 0001767 73.4499 286.6823 13.10379951 02
| Epoch (UTC): | 25 May 2026 15:57:49 |
| Eccentricity: | 0.0001767 |
| inclination: | 87.8865° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7347° |
| argument of perigee: | 73.4499° |
| revolutions per day: | 13.10379951 |
| mean anomaly at epoch: | 286.6823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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