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 28371U 04025F 24357.93028329 .00000877 00000-0 20961-3 0 9992
2 28371 98.5078 334.3507 0025377 156.8673 203.3673 14.56007049 87000
| Epoch (UTC): | 22 December 2024 22:19:36 |
| Eccentricity: | 0.0025377 |
| inclination: | 98.5078° |
| perigee height: | 688 km |
| apogee height: | 724 km |
| right ascension of ascending node: | 334.3507° |
| argument of perigee: | 156.8673° |
| revolutions per day: | 14.56007049 |
| mean anomaly at epoch: | 203.3673° |
| orbit number at epoch: | 8700 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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