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 39439U 13066Z 24280.88001339 .00054107 00000-0 35837-2 0 9997
2 39439 97.7235 244.0075 0042391 115.1584 245.4048 15.06354173588743
| Epoch (UTC): | 06 October 2024 21:07:13 |
| Eccentricity: | 0.0042391 |
| inclination: | 97.7235° |
| perigee height: | 518 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 244.0075° |
| argument of perigee: | 115.1584° |
| revolutions per day: | 15.06354173 |
| mean anomaly at epoch: | 245.4048° |
| orbit number at epoch: | 58874 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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