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 22176.13737310 .00000150 00000-0 80808-4 0 9998
2 25338 98.6430 205.5724 0009145 275.7882 84.2255 14.26142392254366
| Epoch (UTC): | 25 June 2022 03:17:49 |
| Eccentricity: | 0.0009145 |
| inclination: | 98.6430° |
| perigee height: | 798 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 205.5724° |
| argument of perigee: | 275.7882° |
| revolutions per day: | 14.26142392 |
| mean anomaly at epoch: | 84.2255° |
| orbit number at epoch: | 25436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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