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 37789U 26145.62397428 +.00000000 +00000-0 +50358-4 0 00001
2 37789 97.8767 123.5532 0029464 191.7945 290.3813 14.70494027 06
| Epoch (UTC): | 25 May 2026 14:58:31 |
| Eccentricity: | 0.0029464 |
| inclination: | 97.8767° |
| perigee height: | 639 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 123.5532° |
| argument of perigee: | 191.7945° |
| revolutions per day: | 14.70494027 |
| mean anomaly at epoch: | 290.3813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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