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 58818U 26087.99201476 +.00000000 +00000-0 +77079-4 0 00008
2 58818 64.5025 307.2767 0040650 259.1027 100.5484 14.44261246 03
| Epoch (UTC): | 28 March 2026 23:48:30 |
| Eccentricity: | 0.0040650 |
| inclination: | 64.5025° |
| perigee height: | 716 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 307.2767° |
| argument of perigee: | 259.1027° |
| revolutions per day: | 14.44261246 |
| mean anomaly at epoch: | 100.5484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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