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 69032U 26145.58335647 +.00000000 +00000-0 -32952-1 0 00005
2 69032 97.2849 0.3398 0001801 103.6152 168.2376 15.62682540 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001801 |
| inclination: | 97.2849° |
| perigee height: | 379 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 0.3398° |
| argument of perigee: | 103.6152° |
| revolutions per day: | 15.62682540 |
| mean anomaly at epoch: | 168.2376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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