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 26065.57640260 +.00000000 +00000-0 +34660-3 0 00005
2 27651 39.9901 126.8460 0016241 31.2906 328.8852 15.03070095 02
| Epoch (UTC): | 06 March 2026 13:50:01 |
| Eccentricity: | 0.0016241 |
| inclination: | 39.9901° |
| perigee height: | 546 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 126.8460° |
| argument of perigee: | 31.2906° |
| revolutions per day: | 15.03070095 |
| mean anomaly at epoch: | 328.8852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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