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 26066.13061251 +.00000000 +00000-0 +46704-3 0 00003
2 39429 97.6764 291.1544 0115006 356.5198 3.5199 14.75651126 09
| Epoch (UTC): | 07 March 2026 03:08:04 |
| Eccentricity: | 0.0115006 |
| inclination: | 97.6764° |
| perigee height: | 562 km |
| apogee height: | 724 km |
| right ascension of ascending node: | 291.1544° |
| argument of perigee: | 356.5198° |
| revolutions per day: | 14.75651126 |
| mean anomaly at epoch: | 3.5199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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