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 26106.82803809 +.00000000 +00000-0 +12396-3 0 00009
2 39430 97.6536 311.1527 0127565 274.7470 83.9179 14.69235408 03
| Epoch (UTC): | 16 April 2026 19:52:22 |
| Eccentricity: | 0.0127565 |
| inclination: | 97.6536° |
| perigee height: | 574 km |
| apogee height: | 753 km |
| right ascension of ascending node: | 311.1527° |
| argument of perigee: | 274.7470° |
| revolutions per day: | 14.69235408 |
| mean anomaly at epoch: | 83.9179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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