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 30028U 99025ND 24357.92026519 .00004558 00000-0 90427-3 0 9990
2 30028 98.1282 353.7100 0181107 247.3852 172.0069 14.52783219945659
| Epoch (UTC): | 22 December 2024 22:05:10 |
| Eccentricity: | 0.0181107 |
| inclination: | 98.1282° |
| perigee height: | 588 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 353.7100° |
| argument of perigee: | 247.3852° |
| revolutions per day: | 14.52783219 |
| mean anomaly at epoch: | 172.0069° |
| orbit number at epoch: | 94565 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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