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 51105U 26145.41977472 +.00000000 +00000-0 +17082-3 0 00005
2 51105 53.2136 304.6663 0001225 110.3072 249.8052 15.08851872 01
| Epoch (UTC): | 25 May 2026 10:04:28 |
| Eccentricity: | 0.0001225 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 304.6663° |
| argument of perigee: | 110.3072° |
| revolutions per day: | 15.08851872 |
| mean anomaly at epoch: | 249.8052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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