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 37388U 26088.20548270 +.00000000 +00000-0 +13572-3 0 00005
2 37388 98.3623 65.8959 0013720 213.0340 158.4931 14.25593621 09
| Epoch (UTC): | 29 March 2026 04:55:53 |
| Eccentricity: | 0.0013720 |
| inclination: | 98.3623° |
| perigee height: | 797 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 65.8959° |
| argument of perigee: | 213.0340° |
| revolutions per day: | 14.25593621 |
| mean anomaly at epoch: | 158.4931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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