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 62841U 26145.52774698 +.00000000 +00000-0 +77456-3 0 00002
2 62841 42.9982 202.9811 0001407 255.7310 104.3401 15.70863921 00
| Epoch (UTC): | 25 May 2026 12:39:57 |
| Eccentricity: | 0.0001407 |
| inclination: | 42.9982° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 202.9811° |
| argument of perigee: | 255.7310° |
| revolutions per day: | 15.70863921 |
| mean anomaly at epoch: | 104.3401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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