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 29U 60002B 23029.27340037 .00000763 00000-0 14247-3 0 9998
2 29 48.3794 116.5994 0023825 1.3357 358.7615 14.74958554359703
| Epoch (UTC): | 29 January 2023 06:33:41 |
| Eccentricity: | 0.0023825 |
| inclination: | 48.3794° |
| perigee height: | 628 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 116.5994° |
| argument of perigee: | 1.3357° |
| revolutions per day: | 14.74958554 |
| mean anomaly at epoch: | 358.7615° |
| orbit number at epoch: | 35970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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