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 36290U 08053L 24354.75808804 .00004701 00000-0 32550-3 0 9994
2 36290 97.7996 356.9379 0008944 321.2699 38.7885 15.06135383647188
| Epoch (UTC): | 19 December 2024 18:11:38 |
| Eccentricity: | 0.0008944 |
| inclination: | 97.7996° |
| perigee height: | 542 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 356.9379° |
| argument of perigee: | 321.2699° |
| revolutions per day: | 15.06135383 |
| mean anomaly at epoch: | 38.7885° |
| orbit number at epoch: | 64718 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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