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 21014U 90111A 24358.02498289 .00000309 00000-0 11945-3 0 9999
2 21014 74.0452 214.7378 0027643 179.9172 180.1990 14.34039833779944
| Epoch (UTC): | 23 December 2024 00:35:58 |
| Eccentricity: | 0.0027643 |
| inclination: | 74.0452° |
| perigee height: | 758 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 214.7378° |
| argument of perigee: | 179.9172° |
| revolutions per day: | 14.34039833 |
| mean anomaly at epoch: | 180.1990° |
| orbit number at epoch: | 77994 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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