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 54198U 26145.61800705 +.00000000 +00000-0 +51440-4 0 00003
2 54198 53.2126 8.6210 0001183 88.7827 271.3300 15.08840188 07
| Epoch (UTC): | 25 May 2026 14:49:55 |
| Eccentricity: | 0.0001183 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 8.6210° |
| argument of perigee: | 88.7827° |
| revolutions per day: | 15.08840188 |
| mean anomaly at epoch: | 271.3300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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