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 data is extracted from the following two-line orbital elements,
1 36288U 10001B 25073.18137108 .00006268 00000-0 18447-2 0 9993
2 36288 19.7409 153.5078 6987098 135.3357 308.5300 2.65140043135937
| Epoch (UTC): | 14 March 2025 04:21:10 |
| Eccentricity: | 0.6987098 |
| inclination: | 19.7409° |
| perigee height: | 265 km |
| apogee height: | 31079 km |
| right ascension of ascending node: | 153.5078° |
| argument of perigee: | 135.3357° |
| revolutions per day: | 2.65140043 |
| mean anomaly at epoch: | 308.5300° |
| orbit number at epoch: | 13593 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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