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 62429U 26145.31864404 +.00000000 +00000-0 +79712-3 0 00003
2 62429 43.0000 241.2606 0001356 277.6373 82.4324 15.27596234 00
| Epoch (UTC): | 25 May 2026 07:38:50 |
| Eccentricity: | 0.0001356 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 241.2606° |
| argument of perigee: | 277.6373° |
| revolutions per day: | 15.27596234 |
| mean anomaly at epoch: | 82.4324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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