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 26041.16592712 +.00000000 +00000-0 +13126-3 0 00000
2 00005 34.2619 346.3251 1839235 285.7368 54.8649 10.85948196 03
| Epoch (UTC): | 10 February 2026 03:58:56 |
| Eccentricity: | 0.1839235 |
| inclination: | 34.2619° |
| perigee height: | 651 km |
| apogee height: | 3820 km |
| right ascension of ascending node: | 346.3251° |
| argument of perigee: | 285.7368° |
| revolutions per day: | 10.85948196 |
| mean anomaly at epoch: | 54.8649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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