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 54761U 26145.05041370 +.00000000 +00000-0 -61822-4 0 00008
2 54761 53.2139 61.5508 0001720 88.2838 271.8351 15.08843806 00
| Epoch (UTC): | 25 May 2026 01:12:35 |
| Eccentricity: | 0.0001720 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 61.5508° |
| argument of perigee: | 88.2838° |
| revolutions per day: | 15.08843806 |
| mean anomaly at epoch: | 271.8351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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