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 51112U 26145.46856880 +.00000000 +00000-0 +25014-3 0 00001
2 51112 53.2126 304.4167 0001431 101.8144 258.3009 15.08818085 05
| Epoch (UTC): | 25 May 2026 11:14:44 |
| Eccentricity: | 0.0001431 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 304.4167° |
| argument of perigee: | 101.8144° |
| revolutions per day: | 15.08818085 |
| mean anomaly at epoch: | 258.3009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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