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 26069.98269133 +.00000000 +00000-0 +31764-3 0 00000
2 39430 97.6570 276.6073 0130189 33.3989 327.5345 14.69104276 02
| Epoch (UTC): | 10 March 2026 23:35:04 |
| Eccentricity: | 0.0130189 |
| inclination: | 97.6570° |
| perigee height: | 572 km |
| apogee height: | 756 km |
| right ascension of ascending node: | 276.6073° |
| argument of perigee: | 33.3989° |
| revolutions per day: | 14.69104276 |
| mean anomaly at epoch: | 327.5345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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