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 20929U 90095A 23086.53974067 -.00000219 00000-0 00000-0 0 9998
2 20929 14.7380 352.4258 0007242 67.7633 292.2920 0.98399010 13877
| Epoch (UTC): | 27 March 2023 12:57:13 |
| Eccentricity: | 0.0007242 |
| inclination: | 14.7380° |
| perigee height: | 36288 km |
| apogee height: | 36350 km |
| right ascension of ascending node: | 352.4258° |
| argument of perigee: | 67.7633° |
| revolutions per day: | 0.98399010 |
| mean anomaly at epoch: | 292.2920° |
| orbit number at epoch: | 1387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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