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 36288U 10001B 23032.43600647 .00003019 00000-0 18328-2 0 9996
2 36288 19.8815 145.2915 7055097 218.9761 59.2793 2.54022875115945
| Epoch (UTC): | 01 February 2023 10:27:50 |
| Eccentricity: | 0.7055097 |
| inclination: | 19.8815° |
| perigee height: | 303 km |
| apogee height: | 32318 km |
| right ascension of ascending node: | 145.2915° |
| argument of perigee: | 218.9761° |
| revolutions per day: | 2.54022875 |
| mean anomaly at epoch: | 59.2793° |
| orbit number at epoch: | 11594 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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