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 06155U 26074.90961031 +.00000000 +00000-0 +16304-3 0 00005
2 06155 35.0009 269.3023 0032974 61.7647 298.6376 14.77704903 00
| Epoch (UTC): | 15 March 2026 21:49:50 |
| Eccentricity: | 0.0032974 |
| inclination: | 35.0009° |
| perigee height: | 613 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 269.3023° |
| argument of perigee: | 61.7647° |
| revolutions per day: | 14.77704903 |
| mean anomaly at epoch: | 298.6376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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