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 67755U 26143.18199062 +.00000000 +00000-0 +57751-3 0 00003
2 67755 97.3901 220.2671 0005377 105.9823 254.2018 15.43709463 05
| Epoch (UTC): | 23 May 2026 04:22:03 |
| Eccentricity: | 0.0005377 |
| inclination: | 97.3901° |
| perigee height: | 432 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 220.2671° |
| argument of perigee: | 105.9823° |
| revolutions per day: | 15.43709463 |
| mean anomaly at epoch: | 254.2018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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