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 51622U 26145.58829826 +.00000000 +00000-0 -61369-4 0 00005
2 51622 87.9164 10.3492 0003068 97.0860 263.0621 13.17650440 00
| Epoch (UTC): | 25 May 2026 14:07:08 |
| Eccentricity: | 0.0003068 |
| inclination: | 87.9164° |
| perigee height: | 1191 km |
| apogee height: | 1196 km |
| right ascension of ascending node: | 10.3492° |
| argument of perigee: | 97.0860° |
| revolutions per day: | 13.17650440 |
| mean anomaly at epoch: | 263.0621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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