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 00020U 59007A 22274.48124028 .00000575 00000-0 23861-3 0 9999
2 00020 33.3428 82.6112 1664195 23.1718 343.5876 11.56272141327368
| Epoch (UTC): | 01 October 2022 11:32:59 |
| Eccentricity: | 0.1664195 |
| inclination: | 33.3428° |
| perigee height: | 508 km |
| apogee height: | 3257 km |
| right ascension of ascending node: | 82.6112° |
| argument of perigee: | 23.1718° |
| revolutions per day: | 11.56272141 |
| mean anomaly at epoch: | 343.5876° |
| orbit number at epoch: | 32736 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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