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 13124U 26148.61458265 +.00000000 +00000-0 +00000-0 0 00002
2 13124 71.8126 146.2177 4863086 332.9119 250.5817 2.00392917 00
| Epoch (UTC): | 28 May 2026 14:44:59 |
| Eccentricity: | 0.4863086 |
| inclination: | 71.8126° |
| perigee height: | 7273 km |
| apogee height: | 33121 km |
| right ascension of ascending node: | 146.2177° |
| argument of perigee: | 332.9119° |
| revolutions per day: | 2.00392917 |
| mean anomaly at epoch: | 250.5817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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