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 62219U 26145.55811288 +.00000000 +00000-0 +11937-2 0 00002
2 62219 53.1574 82.4028 0000297 23.5811 336.5220 15.69762926 03
| Epoch (UTC): | 25 May 2026 13:23:40 |
| Eccentricity: | 0.0000297 |
| inclination: | 53.1574° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 82.4028° |
| argument of perigee: | 23.5811° |
| revolutions per day: | 15.69762926 |
| mean anomaly at epoch: | 336.5220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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