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 24357.90424910 .00072974 00000-0 19308-2 0 9991
2 32788 97.6056 341.2652 0002298 131.2539 228.8903 15.38117618907101
| Epoch (UTC): | 22 December 2024 21:42:07 |
| Eccentricity: | 0.0002298 |
| inclination: | 97.6056° |
| perigee height: | 450 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 341.2652° |
| argument of perigee: | 131.2539° |
| revolutions per day: | 15.38117618 |
| mean anomaly at epoch: | 228.8903° |
| orbit number at epoch: | 90710 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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