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 62074U 26145.43871160 +.00000000 +00000-0 +68451-3 0 00007
2 62074 53.1582 197.2851 0000928 69.6410 290.4693 15.34406467 06
| Epoch (UTC): | 25 May 2026 10:31:44 |
| Eccentricity: | 0.0000928 |
| inclination: | 53.1582° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 197.2851° |
| argument of perigee: | 69.6410° |
| revolutions per day: | 15.34406467 |
| mean anomaly at epoch: | 290.4693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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