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 25397U 98043D 22180.86763438 .00000005 00000-0 22009-4 0 9990
2 25397 98.8184 131.3688 0002400 79.4551 280.6898 14.23759243245195
| Epoch (UTC): | 29 June 2022 20:49:23 |
| Eccentricity: | 0.0002400 |
| inclination: | 98.8184° |
| perigee height: | 811 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 131.3688° |
| argument of perigee: | 79.4551° |
| revolutions per day: | 14.23759243 |
| mean anomaly at epoch: | 280.6898° |
| orbit number at epoch: | 24519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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