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 23967U 96042A 23342.81088062 .00000106 00000-0 00000+0 0 9991
2 23967 10.2535 21.4733 0006017 101.1211 75.8073 1.00306571100257
| Epoch (UTC): | 08 December 2023 19:27:40 |
| Eccentricity: | 0.0006017 |
| inclination: | 10.2535° |
| perigee height: | 35751 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 21.4733° |
| argument of perigee: | 101.1211° |
| revolutions per day: | 1.00306571 |
| mean anomaly at epoch: | 75.8073° |
| orbit number at epoch: | 10025 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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