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 55375U 26145.58445139 +.00000000 +00000-0 +51854-4 0 00002
2 55375 43.0021 247.2300 0001593 267.1498 92.9171 15.27575955 00
| Epoch (UTC): | 25 May 2026 14:01:36 |
| Eccentricity: | 0.0001593 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.2300° |
| argument of perigee: | 267.1498° |
| revolutions per day: | 15.27575955 |
| mean anomaly at epoch: | 92.9171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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