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 51113U 26145.46024867 +.00000000 +00000-0 +22551-4 0 00008
2 51113 53.2142 304.4820 0001190 89.9985 270.1144 15.08836485 07
| Epoch (UTC): | 25 May 2026 11:02:45 |
| Eccentricity: | 0.0001190 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 304.4820° |
| argument of perigee: | 89.9985° |
| revolutions per day: | 15.08836485 |
| mean anomaly at epoch: | 270.1144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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