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 51794U 26145.66668980 +.00000000 +00000-0 +12548-1 0 00007
2 51794 53.2175 356.9126 0000969 94.7401 84.1148 15.53428286 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000969 |
| inclination: | 53.2175° |
| perigee height: | 406 km |
| apogee height: | 407 km |
| right ascension of ascending node: | 356.9126° |
| argument of perigee: | 94.7401° |
| revolutions per day: | 15.53428286 |
| mean anomaly at epoch: | 84.1148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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