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 22829U 93061G 23332.75215073 .00000306 00000-0 13258-3 0 9996
2 22829 98.7971 18.6897 0008823 240.0003 120.0304 14.31363633574778
| Epoch (UTC): | 28 November 2023 18:03:05 |
| Eccentricity: | 0.0008823 |
| inclination: | 98.7971° |
| perigee height: | 781 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 18.6897° |
| argument of perigee: | 240.0003° |
| revolutions per day: | 14.31363633 |
| mean anomaly at epoch: | 120.0304° |
| orbit number at epoch: | 57477 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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