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 21152U 91019A 23338.33548466 .00000108 00000-0 97353-4 0 9999
2 21152 82.9266 270.4992 0042537 134.8868 342.7686 13.74352875640975
| Epoch (UTC): | 04 December 2023 08:03:05 |
| Eccentricity: | 0.0042537 |
| inclination: | 82.9266° |
| perigee height: | 952 km |
| apogee height: | 1015 km |
| right ascension of ascending node: | 270.4992° |
| argument of perigee: | 134.8868° |
| revolutions per day: | 13.74352875 |
| mean anomaly at epoch: | 342.7686° |
| orbit number at epoch: | 64097 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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