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 26108.89388397 +.00000000 +00000-0 +12016-3 0 00005
2 06155 35.0017 70.1163 0033590 347.4476 12.5386 14.77794850 05
| Epoch (UTC): | 18 April 2026 21:27:11 |
| Eccentricity: | 0.0033590 |
| inclination: | 35.0017° |
| perigee height: | 613 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 70.1163° |
| argument of perigee: | 347.4476° |
| revolutions per day: | 14.77794850 |
| mean anomaly at epoch: | 12.5386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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