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 00029U 60002B 23029.61212090 .00000729 00000-0 13752-3 0 9995
2 00029 48.3794 114.9995 0023813 2.8074 357.2968 14.74959186359645
| Epoch (UTC): | 29 January 2023 14:41:27 |
| Eccentricity: | 0.0023813 |
| inclination: | 48.3794° |
| perigee height: | 628 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 114.9995° |
| argument of perigee: | 2.8074° |
| revolutions per day: | 14.74959186 |
| mean anomaly at epoch: | 357.2968° |
| orbit number at epoch: | 35964 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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