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 62830U 26145.51713003 +.00000000 +00000-0 +81652-3 0 00005
2 62830 43.0016 202.9014 0001381 253.8360 106.2356 15.70844844 01
| Epoch (UTC): | 25 May 2026 12:24:40 |
| Eccentricity: | 0.0001381 |
| inclination: | 43.0016° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 202.9014° |
| argument of perigee: | 253.8360° |
| revolutions per day: | 15.70844844 |
| mean anomaly at epoch: | 106.2356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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