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 23687U 95055B 22138.03673610 .00000253 00000-0 18537-2 0 9998
2 23687 4.8563 99.7068 7245035 305.3099 6.9521 2.21807114214903
| Epoch (UTC): | 18 May 2022 00:52:53 |
| Eccentricity: | 0.7245035 |
| inclination: | 4.8563° |
| perigee height: | 464 km |
| apogee height: | 36451 km |
| right ascension of ascending node: | 99.7068° |
| argument of perigee: | 305.3099° |
| revolutions per day: | 2.21807114 |
| mean anomaly at epoch: | 6.9521° |
| orbit number at epoch: | 21490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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