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 26046.14343162 +.00000000 +00000-0 +30756-3 0 00008
2 39430 97.6583 254.2527 0130764 109.1693 252.3720 14.69001064 08
| Epoch (UTC): | 15 February 2026 03:26:32 |
| Eccentricity: | 0.0130764 |
| inclination: | 97.6583° |
| perigee height: | 572 km |
| apogee height: | 756 km |
| right ascension of ascending node: | 254.2527° |
| argument of perigee: | 109.1693° |
| revolutions per day: | 14.69001064 |
| mean anomaly at epoch: | 252.3720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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