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 62202U 26145.48700807 +.00000000 +00000-0 +49729-3 0 00001
2 62202 42.9991 197.2484 0001391 277.2809 82.7884 15.27590592 04
| Epoch (UTC): | 25 May 2026 11:41:17 |
| Eccentricity: | 0.0001391 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.2484° |
| argument of perigee: | 277.2809° |
| revolutions per day: | 15.27590592 |
| mean anomaly at epoch: | 82.7884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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