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 62303U 26145.48070355 +.00000000 +00000-0 +29709-3 0 00007
2 62303 53.1577 184.2626 0001225 66.5009 293.6121 15.30209499 05
| Epoch (UTC): | 25 May 2026 11:32:12 |
| Eccentricity: | 0.0001225 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.2626° |
| argument of perigee: | 66.5009° |
| revolutions per day: | 15.30209499 |
| mean anomaly at epoch: | 293.6121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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