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 54006U 26145.49469340 +.00000000 +00000-0 +46746-4 0 00006
2 54006 53.2140 228.9024 0001175 86.5616 273.5510 15.08841275 09
| Epoch (UTC): | 25 May 2026 11:52:21 |
| Eccentricity: | 0.0001175 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 228.9024° |
| argument of perigee: | 86.5616° |
| revolutions per day: | 15.08841275 |
| mean anomaly at epoch: | 273.5510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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