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 29252U 06029A 24281.82866067 .00068040 00000-0 13218-2 0 9992
2 29252 64.5112 143.8938 0032646 306.5543 53.2589 15.46638144 8028
| Epoch (UTC): | 07 October 2024 19:53:16 |
| Eccentricity: | 0.0032646 |
| inclination: | 64.5112° |
| perigee height: | 404 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 143.8938° |
| argument of perigee: | 306.5543° |
| revolutions per day: | 15.46638144 |
| mean anomaly at epoch: | 53.2589° |
| orbit number at epoch: | 802 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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