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 58987U 26145.13464919 +.00000000 +00000-0 +60653-4 0 00009
2 58987 97.9976 200.3368 0003621 134.5091 225.6411 14.68262185 07
| Epoch (UTC): | 25 May 2026 03:13:53 |
| Eccentricity: | 0.0003621 |
| inclination: | 97.9976° |
| perigee height: | 664 km |
| apogee height: | 669 km |
| right ascension of ascending node: | 200.3368° |
| argument of perigee: | 134.5091° |
| revolutions per day: | 14.68262185 |
| mean anomaly at epoch: | 225.6411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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