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 54075U 26145.29001263 +.00000000 +00000-0 +31212-3 0 00007
2 54075 53.2127 354.8645 0001193 94.5316 265.5812 15.08810115 09
| Epoch (UTC): | 25 May 2026 06:57:37 |
| Eccentricity: | 0.0001193 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 354.8645° |
| argument of perigee: | 94.5316° |
| revolutions per day: | 15.08810115 |
| mean anomaly at epoch: | 265.5812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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