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 69085U 26144.75935918 +.00000000 +00000-0 -98525+0 0 00004
2 69085 88.9863 344.2949 0016955 218.3690 141.6294 14.18380591 09
| Epoch (UTC): | 24 May 2026 18:13:28 |
| Eccentricity: | 0.0016955 |
| inclination: | 88.9863° |
| perigee height: | 819 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 344.2949° |
| argument of perigee: | 218.3690° |
| revolutions per day: | 14.18380591 |
| mean anomaly at epoch: | 141.6294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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