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 62207U 26145.41568338 +.00000000 +00000-0 +51696-3 0 00006
2 62207 42.9979 194.1179 0001295 268.1318 91.9385 15.27591282 04
| Epoch (UTC): | 25 May 2026 09:58:35 |
| Eccentricity: | 0.0001295 |
| inclination: | 42.9979° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 194.1179° |
| argument of perigee: | 268.1318° |
| revolutions per day: | 15.27591282 |
| mean anomaly at epoch: | 91.9385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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