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 59051U 26145.60362030 +.00000000 +00000-0 +20780-4 0 00002
2 59051 98.7000 105.1874 0006092 229.8352 130.2293 14.22426863 08
| Epoch (UTC): | 25 May 2026 14:29:12 |
| Eccentricity: | 0.0006092 |
| inclination: | 98.7000° |
| perigee height: | 813 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 105.1874° |
| argument of perigee: | 229.8352° |
| revolutions per day: | 14.22426863 |
| mean anomaly at epoch: | 130.2293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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