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 00059U 60013B 23030.14229533 .00000149 00000-0 84613-4 0 9991
2 00059 28.2502 343.8047 0189124 36.1606 325.1567 13.53016614 75901
| Epoch (UTC): | 30 January 2023 03:24:54 |
| Eccentricity: | 0.0189124 |
| inclination: | 28.2502° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 343.8047° |
| argument of perigee: | 36.1606° |
| revolutions per day: | 13.53016614 |
| mean anomaly at epoch: | 325.1567° |
| orbit number at epoch: | 7590 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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