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 22175.85673692 .00000146 00000-0 79456-4 0 9990
2 25338 98.6430 205.2955 0009144 276.7250 83.2889 14.26142218254075
| Epoch (UTC): | 24 June 2022 20:33:42 |
| Eccentricity: | 0.0009144 |
| inclination: | 98.6430° |
| perigee height: | 798 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 205.2955° |
| argument of perigee: | 276.7250° |
| revolutions per day: | 14.26142218 |
| mean anomaly at epoch: | 83.2889° |
| orbit number at epoch: | 25407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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