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 25338U 98030A 22183.15327310 .00000126 00000-0 71098-4 0 9997
2 25338 98.6427 212.4959 0009212 252.6451 107.3722 14.26144988255360
| Epoch (UTC): | 02 July 2022 03:40:42 |
| Eccentricity: | 0.0009212 |
| inclination: | 98.6427° |
| perigee height: | 798 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 212.4959° |
| argument of perigee: | 252.6451° |
| revolutions per day: | 14.26144988 |
| mean anomaly at epoch: | 107.3722° |
| orbit number at epoch: | 25536 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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