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 39433U 26068.77891091 +.00000000 +00000-0 +14695-2 0 00006
2 39433 97.4699 82.1645 0007751 211.8767 148.2059 16.31051261 01
| Epoch (UTC): | 09 March 2026 18:41:37 |
| Eccentricity: | 0.0007751 |
| inclination: | 97.4699° |
| perigee height: | 185 km |
| apogee height: | 195 km |
| right ascension of ascending node: | 82.1645° |
| argument of perigee: | 211.8767° |
| revolutions per day: | 16.31051261 |
| mean anomaly at epoch: | 148.2059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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