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 55612U 26145.64300863 +.00000000 +00000-0 +30585-5 0 00006
2 55612 43.0053 280.0408 0002059 273.2382 86.8234 15.26743953 07
| Epoch (UTC): | 25 May 2026 15:25:55 |
| Eccentricity: | 0.0002059 |
| inclination: | 43.0053° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 280.0408° |
| argument of perigee: | 273.2382° |
| revolutions per day: | 15.26743953 |
| mean anomaly at epoch: | 86.8234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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