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 25693U 99021A 24284.40236906 .00002845 00000-0 36262-3 0 9997
2 25693 64.5553 164.1709 0042167 297.1425 62.5383 14.82881526375639
| Epoch (UTC): | 10 October 2024 09:39:24 |
| Eccentricity: | 0.0042167 |
| inclination: | 64.5553° |
| perigee height: | 591 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 164.1709° |
| argument of perigee: | 297.1425° |
| revolutions per day: | 14.82881526 |
| mean anomaly at epoch: | 62.5383° |
| orbit number at epoch: | 37563 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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