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 59377U 26145.35125955 +.00000000 +00000-0 -10364-4 0 00006
2 59377 53.1592 210.9306 0000964 96.5928 263.5183 15.30193778 09
| Epoch (UTC): | 25 May 2026 08:25:48 |
| Eccentricity: | 0.0000964 |
| inclination: | 53.1592° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.9306° |
| argument of perigee: | 96.5928° |
| revolutions per day: | 15.30193778 |
| mean anomaly at epoch: | 263.5183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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