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 29092U 06015A 21055.84810976 .00000137 00000-0 23381-4 0 9992
2 29092 97.9205 84.2896 0001436 91.0255 269.1123 14.83131701802147
| Epoch (UTC): | 24 February 2021 20:21:16 |
| Eccentricity: | 0.0001436 |
| inclination: | 97.9205° |
| perigee height: | 618 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 84.2896° |
| argument of perigee: | 91.0255° |
| revolutions per day: | 14.83131701 |
| mean anomaly at epoch: | 269.1123° |
| orbit number at epoch: | 80214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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