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 19468U 88080B 23150.11882918 .00000389 00000-0 27004-3 0 9997
2 19468 99.1154 189.0920 0072114 144.1075 278.6502 14.03581720778109
| Epoch (UTC): | 30 May 2023 02:51:06 |
| Eccentricity: | 0.0072114 |
| inclination: | 99.1154° |
| perigee height: | 829 km |
| apogee height: | 934 km |
| right ascension of ascending node: | 189.0920° |
| argument of perigee: | 144.1075° |
| revolutions per day: | 14.03581720 |
| mean anomaly at epoch: | 278.6502° |
| orbit number at epoch: | 77810 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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