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 62196U 26145.44874133 +.00000000 +00000-0 +41334-3 0 00007
2 62196 43.0027 164.5508 0001889 266.0104 94.0532 15.27588706 08
| Epoch (UTC): | 25 May 2026 10:46:11 |
| Eccentricity: | 0.0001889 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.5508° |
| argument of perigee: | 266.0104° |
| revolutions per day: | 15.27588706 |
| mean anomaly at epoch: | 94.0532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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