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 43761U 26100.27072663 +.00000000 +00000-0 +21000-3 0 00002
2 43761 97.4253 143.5777 0010782 211.4835 148.5749 15.06270473 02
| Epoch (UTC): | 10 April 2026 06:29:50 |
| Eccentricity: | 0.0010782 |
| inclination: | 97.4253° |
| perigee height: | 540 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 143.5777° |
| argument of perigee: | 211.4835° |
| revolutions per day: | 15.06270473 |
| mean anomaly at epoch: | 148.5749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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