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 24257.59375762 .00001771 00000-0 79851-3 0 9995
2 27844 98.6798 263.4091 0008538 245.3017 114.7273 14.23460994100395
| Epoch (UTC): | 13 September 2024 14:15:00 |
| Eccentricity: | 0.0008538 |
| inclination: | 98.6798° |
| perigee height: | 807 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 263.4091° |
| argument of perigee: | 245.3017° |
| revolutions per day: | 14.23460994 |
| mean anomaly at epoch: | 114.7273° |
| orbit number at epoch: | 10039 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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