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 00005U 26018.45156994 +.00000000 +00000-0 -24507-4 0 00001
2 00005 34.2491 56.4106 1839482 183.3677 175.2761 10.85940622 08
| Epoch (UTC): | 18 January 2026 10:50:15 |
| Eccentricity: | 0.1839482 |
| inclination: | 34.2491° |
| perigee height: | 651 km |
| apogee height: | 3820 km |
| right ascension of ascending node: | 56.4106° |
| argument of perigee: | 183.3677° |
| revolutions per day: | 10.85940622 |
| mean anomaly at epoch: | 175.2761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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