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 54085U 26145.59506990 +.00000000 +00000-0 +26825-4 0 00003
2 54085 53.2116 348.9139 0001314 87.6410 272.4733 15.08835532 02
| Epoch (UTC): | 25 May 2026 14:16:54 |
| Eccentricity: | 0.0001314 |
| inclination: | 53.2116° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 348.9139° |
| argument of perigee: | 87.6410° |
| revolutions per day: | 15.08835532 |
| mean anomaly at epoch: | 272.4733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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