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 51118U 26145.45656582 +.00000000 +00000-0 +33051-4 0 00004
2 51118 53.2129 304.4990 0001229 92.9311 267.1822 15.08838956 09
| Epoch (UTC): | 25 May 2026 10:57:27 |
| Eccentricity: | 0.0001229 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 304.4990° |
| argument of perigee: | 92.9311° |
| revolutions per day: | 15.08838956 |
| mean anomaly at epoch: | 267.1822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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