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 69098U 26135.82925809 +.00000000 +00000-0 +65499-4 0 00002
2 69098 97.5046 218.5086 0013053 280.0851 79.8906 15.10832199 09
| Epoch (UTC): | 15 May 2026 19:54:07 |
| Eccentricity: | 0.0013053 |
| inclination: | 97.5046° |
| perigee height: | 525 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 218.5086° |
| argument of perigee: | 280.0851° |
| revolutions per day: | 15.10832199 |
| mean anomaly at epoch: | 79.8906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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