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 49301U 21090Y 24358.12068749 .00000048 00000-0 85909-4 0 9995
2 49301 87.9249 22.0874 0002460 86.9606 273.1809 13.20770279160395
| Epoch (UTC): | 23 December 2024 02:53:47 |
| Eccentricity: | 0.0002460 |
| inclination: | 87.9249° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 22.0874° |
| argument of perigee: | 86.9606° |
| revolutions per day: | 13.20770279 |
| mean anomaly at epoch: | 273.1809° |
| orbit number at epoch: | 16039 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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