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 69029U 26145.59303374 +.00000000 +00000-0 +61800-3 0 00009
2 69029 97.2848 0.3642 0001375 90.3396 269.8026 15.75216781 03
| Epoch (UTC): | 25 May 2026 14:13:58 |
| Eccentricity: | 0.0001375 |
| inclination: | 97.2848° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 0.3642° |
| argument of perigee: | 90.3396° |
| revolutions per day: | 15.75216781 |
| mean anomaly at epoch: | 269.8026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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