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 23589U 95027A 21015.60737206 -.00000018 00000-0 00000-0 0 9990
2 23589 10.8624 19.7099 0006562 334.0682 21.6720 0.98749873 93454
| Epoch (UTC): | 15 January 2021 14:34:36 |
| Eccentricity: | 0.0006562 |
| inclination: | 10.8624° |
| perigee height: | 36190 km |
| apogee height: | 36246 km |
| right ascension of ascending node: | 19.7099° |
| argument of perigee: | 334.0682° |
| revolutions per day: | 0.98749873 |
| mean anomaly at epoch: | 21.6720° |
| orbit number at epoch: | 9345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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