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 51623U 26145.41117654 +.00000000 +00000-0 -25452-3 0 00009
2 51623 87.8856 40.7993 0001259 83.3500 276.7770 13.10370647 07
| Epoch (UTC): | 25 May 2026 09:52:05 |
| Eccentricity: | 0.0001259 |
| inclination: | 87.8856° |
| perigee height: | 1221 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7993° |
| argument of perigee: | 83.3500° |
| revolutions per day: | 13.10370647 |
| mean anomaly at epoch: | 276.7770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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