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 55376U 26145.46931345 +.00000000 +00000-0 +12859-4 0 00001
2 55376 43.0019 215.2602 0001230 267.8302 92.2408 15.27577918 04
| Epoch (UTC): | 25 May 2026 11:15:48 |
| Eccentricity: | 0.0001230 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.2602° |
| argument of perigee: | 267.8302° |
| revolutions per day: | 15.27577918 |
| mean anomaly at epoch: | 92.2408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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