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 27432U 02024C 24282.57507288 .00000501 00000-0 28163-3 0 9995
2 27432 98.9630 325.3828 0050988 50.7358 73.2225 14.14383043156132
| Epoch (UTC): | 08 October 2024 13:48:06 |
| Eccentricity: | 0.0050988 |
| inclination: | 98.9630° |
| perigee height: | 807 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 325.3828° |
| argument of perigee: | 50.7358° |
| revolutions per day: | 14.14383043 |
| mean anomaly at epoch: | 73.2225° |
| orbit number at epoch: | 15613 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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