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 25991U 99067A 23333.61009691 .00000438 00000-0 24148-3 0 9990
2 25991 99.0719 340.1325 0010835 122.6320 349.8232 14.16856640238830
| Epoch (UTC): | 29 November 2023 14:38:32 |
| Eccentricity: | 0.0010835 |
| inclination: | 99.0719° |
| perigee height: | 828 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 340.1325° |
| argument of perigee: | 122.6320° |
| revolutions per day: | 14.16856640 |
| mean anomaly at epoch: | 349.8232° |
| orbit number at epoch: | 23883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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