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 62255U 26145.65200691 +.00000000 +00000-0 +15099-3 0 00007
2 62255 89.0094 24.4112 0003856 101.4314 258.7270 13.51008171 00
| Epoch (UTC): | 25 May 2026 15:38:53 |
| Eccentricity: | 0.0003856 |
| inclination: | 89.0094° |
| perigee height: | 1066 km |
| apogee height: | 1071 km |
| right ascension of ascending node: | 24.4112° |
| argument of perigee: | 101.4314° |
| revolutions per day: | 13.51008171 |
| mean anomaly at epoch: | 258.7270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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