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 32788U 08021F 24261.18420316 .00103712 00000-0 41468-2 0 9998
2 32788 97.5995 242.1224 0005544 154.0346 206.1170 15.24650419892409
| Epoch (UTC): | 17 September 2024 04:25:15 |
| Eccentricity: | 0.0005544 |
| inclination: | 97.5995° |
| perigee height: | 488 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 242.1224° |
| argument of perigee: | 154.0346° |
| revolutions per day: | 15.24650419 |
| mean anomaly at epoch: | 206.1170° |
| orbit number at epoch: | 89240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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