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 15370U 26156.48275505 +.00000000 +00000-0 +45991-4 0 00007
2 15370 82.5149 173.8414 0021119 45.6741 314.6202 14.86135487 01
| Epoch (UTC): | 05 June 2026 11:35:10 |
| Eccentricity: | 0.0021119 |
| inclination: | 82.5149° |
| perigee height: | 595 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 173.8414° |
| argument of perigee: | 45.6741° |
| revolutions per day: | 14.86135487 |
| mean anomaly at epoch: | 314.6202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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