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 69080U 26145.61695656 +.00000000 +00000-0 +44177-4 0 00005
2 69080 88.9868 344.1993 0004272 153.1706 206.9706 14.19321556 00
| Epoch (UTC): | 25 May 2026 14:48:25 |
| Eccentricity: | 0.0004272 |
| inclination: | 88.9868° |
| perigee height: | 825 km |
| apogee height: | 831 km |
| right ascension of ascending node: | 344.1993° |
| argument of perigee: | 153.1706° |
| revolutions per day: | 14.19321556 |
| mean anomaly at epoch: | 206.9706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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