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 36794U 10034C 24308.60003331 .00004360 00000-0 14068-2 0 9994
2 36794 49.5023 283.2993 5439329 128.6496 294.0250 4.86766562246623
Epoch (UTC): | 03 November 2024 14:24:02 |
Eccentricity: | 0.5439329 |
inclination: | 49.5023° |
perigee height: | 329 km |
apogee height: | 16328 km |
right ascension of ascending node: | 283.2993° |
argument of perigee: | 128.6496° |
revolutions per day: | 4.86766562 |
mean anomaly at epoch: | 294.0250° |
orbit number at epoch: | 24662 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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