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 61981U 26145.60342247 +.00000000 +00000-0 +56466-3 0 00004
2 61981 43.0046 105.3942 0001747 273.4409 86.6243 15.27591941 09
| Epoch (UTC): | 25 May 2026 14:28:55 |
| Eccentricity: | 0.0001747 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 105.3942° |
| argument of perigee: | 273.4409° |
| revolutions per day: | 15.27591941 |
| mean anomaly at epoch: | 86.6243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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