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 27141U 01049CM 24358.10348101 .00004262 00000-0 46162-3 0 9995
2 27141 98.1497 26.2095 0047860 205.1710 222.2929 14.87963692241561
| Epoch (UTC): | 23 December 2024 02:29:00 |
| Eccentricity: | 0.0047860 |
| inclination: | 98.1497° |
| perigee height: | 571 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 26.2095° |
| argument of perigee: | 205.1710° |
| revolutions per day: | 14.87963692 |
| mean anomaly at epoch: | 222.2929° |
| orbit number at epoch: | 24156 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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