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 27651U 26145.09288411 +.00000000 +00000-0 +19459-3 0 00006
2 27651 39.9924 33.4247 0018644 248.3068 111.5741 15.03562587 08
| Epoch (UTC): | 25 May 2026 02:13:45 |
| Eccentricity: | 0.0018644 |
| inclination: | 39.9924° |
| perigee height: | 543 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 33.4247° |
| argument of perigee: | 248.3068° |
| revolutions per day: | 15.03562587 |
| mean anomaly at epoch: | 111.5741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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