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 69043U 26145.58117269 +.00000000 +00000-0 +22398-2 0 00008
2 69043 97.2833 0.3784 0004485 197.2578 162.8536 15.75519200 04
| Epoch (UTC): | 25 May 2026 13:56:53 |
| Eccentricity: | 0.0004485 |
| inclination: | 97.2833° |
| perigee height: | 340 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 0.3784° |
| argument of perigee: | 197.2578° |
| revolutions per day: | 15.75519200 |
| mean anomaly at epoch: | 162.8536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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