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 36501U 26076.29626061 +.00000000 +00000-0 +87309-3 0 00001
2 36501 49.6487 277.1466 4793574 91.7836 321.5800 5.96742017 01
| Epoch (UTC): | 17 March 2026 07:06:36 |
| Eccentricity: | 0.4793574 |
| inclination: | 49.6487° |
| perigee height: | 307 km |
| apogee height: | 12616 km |
| right ascension of ascending node: | 277.1466° |
| argument of perigee: | 91.7836° |
| revolutions per day: | 5.96742017 |
| mean anomaly at epoch: | 321.5800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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