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 69019U 26145.64612529 +.00000000 +00000-0 +12429-3 0 00002
2 69019 97.4064 43.8731 0006747 101.3530 258.8464 15.20371386 03
| Epoch (UTC): | 25 May 2026 15:30:25 |
| Eccentricity: | 0.0006747 |
| inclination: | 97.4064° |
| perigee height: | 500 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 43.8731° |
| argument of perigee: | 101.3530° |
| revolutions per day: | 15.20371386 |
| mean anomaly at epoch: | 258.8464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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