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 32243U 99025CWR 24353.09530984 .00006097 00000-0 29416-2 0 9990
2 32243 98.2969 43.5926 0279728 64.2740 298.7021 14.00477174885461
| Epoch (UTC): | 18 December 2024 02:17:14 |
| Eccentricity: | 0.0279728 |
| inclination: | 98.2969° |
| perigee height: | 689 km |
| apogee height: | 1095 km |
| right ascension of ascending node: | 43.5926° |
| argument of perigee: | 64.2740° |
| revolutions per day: | 14.00477174 |
| mean anomaly at epoch: | 298.7021° |
| orbit number at epoch: | 88546 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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