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 54098U 26145.55830715 +.00000000 +00000-0 +34952-4 0 00008
2 54098 53.2122 349.3786 0001274 90.8622 269.2516 15.08837987 01
| Epoch (UTC): | 25 May 2026 13:23:57 |
| Eccentricity: | 0.0001274 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 349.3786° |
| argument of perigee: | 90.8622° |
| revolutions per day: | 15.08837987 |
| mean anomaly at epoch: | 269.2516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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