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 54200U 26145.61064272 +.00000000 +00000-0 +25819-4 0 00009
2 54200 53.2135 8.5723 0001208 89.5252 270.5878 15.08834338 09
| Epoch (UTC): | 25 May 2026 14:39:19 |
| Eccentricity: | 0.0001208 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 8.5723° |
| argument of perigee: | 89.5252° |
| revolutions per day: | 15.08834338 |
| mean anomaly at epoch: | 270.5878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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