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 37619U 26087.63947394 +.00000000 +00000-0 +30596-3 0 00003
2 37619 98.8909 63.9654 0010239 203.4271 156.6433 14.08318898 06
| Epoch (UTC): | 28 March 2026 15:20:50 |
| Eccentricity: | 0.0010239 |
| inclination: | 98.8909° |
| perigee height: | 858 km |
| apogee height: | 873 km |
| right ascension of ascending node: | 63.9654° |
| argument of perigee: | 203.4271° |
| revolutions per day: | 14.08318898 |
| mean anomaly at epoch: | 156.6433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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