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 39430U 26072.43461115 +.00000000 +00000-0 +24491-3 0 00007
2 39430 97.6572 278.9062 0130010 25.5646 335.1914 14.69112735 09
| Epoch (UTC): | 13 March 2026 10:25:50 |
| Eccentricity: | 0.0130010 |
| inclination: | 97.6572° |
| perigee height: | 572 km |
| apogee height: | 755 km |
| right ascension of ascending node: | 278.9062° |
| argument of perigee: | 25.5646° |
| revolutions per day: | 14.69112735 |
| mean anomaly at epoch: | 335.1914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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