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 27844U 03031E 24259.91336104 .00001574 00000-0 71161-3 0 9997
2 27844 98.6801 265.6977 0008629 237.5634 122.4710 14.23467297100694
| Epoch (UTC): | 15 September 2024 21:55:14 |
| Eccentricity: | 0.0008629 |
| inclination: | 98.6801° |
| perigee height: | 807 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 265.6977° |
| argument of perigee: | 237.5634° |
| revolutions per day: | 14.23467297 |
| mean anomaly at epoch: | 122.4710° |
| orbit number at epoch: | 10069 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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