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 23090.82061021 .00000851 00000-0 39949-3 0 9997
2 27844 98.6808 99.2055 0009672 357.2995 2.8129 14.22705582 24767
| Epoch (UTC): | 31 March 2023 19:41:40 |
| Eccentricity: | 0.0009672 |
| inclination: | 98.6808° |
| perigee height: | 809 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 99.2055° |
| argument of perigee: | 357.2995° |
| revolutions per day: | 14.22705582 |
| mean anomaly at epoch: | 2.8129° |
| orbit number at epoch: | 2476 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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