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 23263.88022624 .00000144 00000-0 69432-4 0 9999
2 00059 28.2476 223.0395 0189162 198.0709 161.3038 13.53040207107588
| Epoch (UTC): | 20 September 2023 21:07:31 |
| Eccentricity: | 0.0189162 |
| inclination: | 28.2476° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 223.0395° |
| argument of perigee: | 198.0709° |
| revolutions per day: | 13.53040207 |
| mean anomaly at epoch: | 161.3038° |
| orbit number at epoch: | 10758 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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