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 41556U 26145.62970102 +.00000000 +00000-0 +23688-3 0 00009
2 41556 97.3838 221.8358 0012999 15.2940 344.8687 15.21219720 01
| Epoch (UTC): | 25 May 2026 15:06:46 |
| Eccentricity: | 0.0012999 |
| inclination: | 97.3838° |
| perigee height: | 493 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 221.8358° |
| argument of perigee: | 15.2940° |
| revolutions per day: | 15.21219720 |
| mean anomaly at epoch: | 344.8687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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