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 32953U 08025A 24262.83132851 .00000022 00000-0 86472-4 0 9999
2 32953 82.5060 31.2259 0018685 259.3921 100.5054 12.43148251740766
| Epoch (UTC): | 18 September 2024 19:57:06 |
| Eccentricity: | 0.0018685 |
| inclination: | 82.5060° |
| perigee height: | 1478 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 31.2259° |
| argument of perigee: | 259.3921° |
| revolutions per day: | 12.43148251 |
| mean anomaly at epoch: | 100.5054° |
| orbit number at epoch: | 74076 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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