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 69027U 26145.53204101 +.00000000 +00000-0 -37779-2 0 00007
2 69027 97.2849 0.2945 0001641 34.0621 326.0749 15.74669637 08
| Epoch (UTC): | 25 May 2026 12:46:08 |
| Eccentricity: | 0.0001641 |
| inclination: | 97.2849° |
| perigee height: | 344 km |
| apogee height: | 347 km |
| right ascension of ascending node: | 0.2945° |
| argument of perigee: | 34.0621° |
| revolutions per day: | 15.74669637 |
| mean anomaly at epoch: | 326.0749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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