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 69034U 26145.58985557 +.00000000 +00000-0 +54395-3 0 00004
2 69034 97.2851 0.3683 0001374 83.5298 276.6123 15.75221737 03
| Epoch (UTC): | 25 May 2026 14:09:23 |
| Eccentricity: | 0.0001374 |
| inclination: | 97.2851° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 0.3683° |
| argument of perigee: | 83.5298° |
| revolutions per day: | 15.75221737 |
| mean anomaly at epoch: | 276.6123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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