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 34223U 02024H 25346.41133501 .00001139 00000-0 68270-3 0 9990
2 34223 99.0829 32.8241 0129440 156.8811 203.8253 14.04935393185113
| Epoch (UTC): | 12 December 2025 09:52:19 |
| Eccentricity: | 0.0129440 |
| inclination: | 99.0829° |
| perigee height: | 783 km |
| apogee height: | 970 km |
| right ascension of ascending node: | 32.8241° |
| argument of perigee: | 156.8811° |
| revolutions per day: | 14.04935393 |
| mean anomaly at epoch: | 203.8253° |
| orbit number at epoch: | 18511 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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