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 00116U 61015A 24250.57114495 .00000285 00000-0 27667-3 0 9996
2 00116 66.8110 37.7124 0074465 2.6986 357.4480 13.92090989206417
| Epoch (UTC): | 06 September 2024 13:42:26 |
| Eccentricity: | 0.0074465 |
| inclination: | 66.8110° |
| perigee height: | 867 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 37.7124° |
| argument of perigee: | 2.6986° |
| revolutions per day: | 13.92090989 |
| mean anomaly at epoch: | 357.4480° |
| orbit number at epoch: | 20641 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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