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 43508U 26144.15229310 +.00000000 +00000-0 +00000-0 0 00003
2 43508 65.5655 74.7084 0007601 245.1002 114.8130 2.13102017 07
| Epoch (UTC): | 24 May 2026 03:39:18 |
| Eccentricity: | 0.0007601 |
| inclination: | 65.5655° |
| perigee height: | 19111 km |
| apogee height: | 19149 km |
| right ascension of ascending node: | 74.7084° |
| argument of perigee: | 245.1002° |
| revolutions per day: | 2.13102017 |
| mean anomaly at epoch: | 114.8130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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