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 51653U 26145.42279068 +.00000000 +00000-0 -15653-2 0 00002
2 51653 87.8851 40.8087 0001923 76.9141 283.2201 13.10372128 05
| Epoch (UTC): | 25 May 2026 10:08:49 |
| Eccentricity: | 0.0001923 |
| inclination: | 87.8851° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8087° |
| argument of perigee: | 76.9141° |
| revolutions per day: | 13.10372128 |
| mean anomaly at epoch: | 283.2201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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