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 28415U 26137.53214301 +.00000000 +00000-0 +19566-3 0 00001
2 28415 97.3388 170.9594 0033120 84.9322 275.5698 15.30119884 04
| Epoch (UTC): | 17 May 2026 12:46:17 |
| Eccentricity: | 0.0033120 |
| inclination: | 97.3388° |
| perigee height: | 453 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 170.9594° |
| argument of perigee: | 84.9322° |
| revolutions per day: | 15.30119884 |
| mean anomaly at epoch: | 275.5698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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