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 69039U 26145.50003470 +.00000000 +00000-0 -17230-1 0 00002
2 69039 97.2850 0.2891 0001651 90.0778 151.8828 15.71072319 03
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001651 |
| inclination: | 97.2850° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 0.2891° |
| argument of perigee: | 90.0778° |
| revolutions per day: | 15.71072319 |
| mean anomaly at epoch: | 151.8828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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