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 54227U 26145.38110552 +.00000000 +00000-0 +17496-3 0 00006
2 54227 97.6822 147.0804 0010558 278.7303 81.2727 15.05189276 00
| Epoch (UTC): | 25 May 2026 09:08:47 |
| Eccentricity: | 0.0010558 |
| inclination: | 97.6822° |
| perigee height: | 544 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 147.0804° |
| argument of perigee: | 278.7303° |
| revolutions per day: | 15.05189276 |
| mean anomaly at epoch: | 81.2727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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