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 54164U 26145.38897277 +.00000000 +00000-0 +49705-5 0 00002
2 54164 53.2126 20.0113 0001120 112.6588 247.4523 15.08836902 02
| Epoch (UTC): | 25 May 2026 09:20:07 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 20.0113° |
| argument of perigee: | 112.6588° |
| revolutions per day: | 15.08836902 |
| mean anomaly at epoch: | 247.4523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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