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 62838U 26145.56569781 +.00000000 +00000-0 +11012-2 0 00002
2 62838 43.0029 202.3905 0001126 268.3479 91.7260 15.70846467 00
| Epoch (UTC): | 25 May 2026 13:34:36 |
| Eccentricity: | 0.0001126 |
| inclination: | 43.0029° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 202.3905° |
| argument of perigee: | 268.3479° |
| revolutions per day: | 15.70846467 |
| mean anomaly at epoch: | 91.7260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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