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 27424U 26145.48766875 +.00000000 +00000-0 +14761-3 0 00003
2 27424 98.4265 114.3197 0001900 64.5333 83.4814 14.62116840 06
| Epoch (UTC): | 25 May 2026 11:42:14 |
| Eccentricity: | 0.0001900 |
| inclination: | 98.4265° |
| perigee height: | 685 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 114.3197° |
| argument of perigee: | 64.5333° |
| revolutions per day: | 14.62116840 |
| mean anomaly at epoch: | 83.4814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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