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 54811U 26145.42855347 +.00000000 +00000-0 +12138-3 0 00006
2 54811 53.2118 39.6696 0001343 82.6426 277.4719 15.08829296 06
| Epoch (UTC): | 25 May 2026 10:17:07 |
| Eccentricity: | 0.0001343 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.6696° |
| argument of perigee: | 82.6426° |
| revolutions per day: | 15.08829296 |
| mean anomaly at epoch: | 277.4719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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