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 25405U 98044B 22147.43122215 .00000039 00000-0 51063-3 0 9997
2 25405 18.3358 171.0146 7138615 184.2814 158.6200 2.25621343196618
| Epoch (UTC): | 27 May 2022 10:20:57 |
| Eccentricity: | 0.7138615 |
| inclination: | 18.3358° |
| perigee height: | 648 km |
| apogee height: | 35706 km |
| right ascension of ascending node: | 171.0146° |
| argument of perigee: | 184.2814° |
| revolutions per day: | 2.25621343 |
| mean anomaly at epoch: | 158.6200° |
| orbit number at epoch: | 19661 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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