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 39429U 26141.04669637 +.00000000 +00000-0 +25045-3 0 00004
2 39429 97.6657 2.2815 0115500 112.4541 248.8950 14.76075224 01
| Epoch (UTC): | 21 May 2026 01:07:14 |
| Eccentricity: | 0.0115500 |
| inclination: | 97.6657° |
| perigee height: | 561 km |
| apogee height: | 723 km |
| right ascension of ascending node: | 2.2815° |
| argument of perigee: | 112.4541° |
| revolutions per day: | 14.76075224 |
| mean anomaly at epoch: | 248.8950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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