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 69048U 26145.58335647 +.00000000 +00000-0 -22977-1 0 00008
2 69048 97.2844 0.3929 0001763 73.0357 318.3302 15.71685832 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001763 |
| inclination: | 97.2844° |
| perigee height: | 353 km |
| apogee height: | 355 km |
| right ascension of ascending node: | 0.3929° |
| argument of perigee: | 73.0357° |
| revolutions per day: | 15.71685832 |
| mean anomaly at epoch: | 318.3302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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