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 25348.27613775 .00000507 00000-0 23886-3 0 9994
2 27844 98.6765 354.1593 0009711 9.0596 351.0757 14.24180797165356
| Epoch (UTC): | 14 December 2025 06:37:38 |
| Eccentricity: | 0.0009711 |
| inclination: | 98.6765° |
| perigee height: | 804 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 354.1593° |
| argument of perigee: | 9.0596° |
| revolutions per day: | 14.24180797 |
| mean anomaly at epoch: | 351.0757° |
| orbit number at epoch: | 16535 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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