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 25135.18013104 .00000718 00000-0 12744-3 0 9990
2 29 48.3771 114.9671 0022640 353.4898 6.5718 14.77962192483354
| Epoch (UTC): | 15 May 2025 04:19:23 |
| Eccentricity: | 0.0022640 |
| inclination: | 48.3771° |
| perigee height: | 620 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 114.9671° |
| argument of perigee: | 353.4898° |
| revolutions per day: | 14.77962192 |
| mean anomaly at epoch: | 6.5718° |
| orbit number at epoch: | 48335 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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