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 07714U 75023A 22229.33081411 .00000272 00000-0 15177-3 0 9999
2 07714 81.2142 154.0791 0029485 342.5722 17.4433 14.08095546750500
| Epoch (UTC): | 17 August 2022 07:56:22 |
| Eccentricity: | 0.0029485 |
| inclination: | 81.2142° |
| perigee height: | 844 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 154.0791° |
| argument of perigee: | 342.5722° |
| revolutions per day: | 14.08095546 |
| mean anomaly at epoch: | 17.4433° |
| orbit number at epoch: | 75050 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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