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 54209U 26145.60050605 +.00000000 +00000-0 +43719-4 0 00001
2 54209 53.2126 358.5150 0001115 109.9989 250.1123 15.08843121 08
| Epoch (UTC): | 25 May 2026 14:24:43 |
| Eccentricity: | 0.0001115 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 358.5150° |
| argument of perigee: | 109.9989° |
| revolutions per day: | 15.08843121 |
| mean anomaly at epoch: | 250.1123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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