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 58828U 26145.45172007 +.00000000 +00000-0 +10279-4 0 00001
2 58828 53.1597 207.4260 0001049 80.6109 279.5010 15.30191818 03
| Epoch (UTC): | 25 May 2026 10:50:28 |
| Eccentricity: | 0.0001049 |
| inclination: | 53.1597° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.4260° |
| argument of perigee: | 80.6109° |
| revolutions per day: | 15.30191818 |
| mean anomaly at epoch: | 279.5010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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