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 69084U 26145.60805470 +.00000000 +00000-0 +32152-4 0 00005
2 69084 88.9868 344.1980 0002967 173.8366 186.2862 14.20799018 07
| Epoch (UTC): | 25 May 2026 14:35:35 |
| Eccentricity: | 0.0002967 |
| inclination: | 88.9868° |
| perigee height: | 821 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 344.1980° |
| argument of perigee: | 173.8366° |
| revolutions per day: | 14.20799018 |
| mean anomaly at epoch: | 186.2862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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