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 25344.86660307 .00001097 00000-0 17734-3 0 9995
2 29 48.3767 199.4170 0022433 178.6234 181.4745 14.78412080514267
| Epoch (UTC): | 10 December 2025 20:47:54 |
| Eccentricity: | 0.0022433 |
| inclination: | 48.3767° |
| perigee height: | 618 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 199.4170° |
| argument of perigee: | 178.6234° |
| revolutions per day: | 14.78412080 |
| mean anomaly at epoch: | 181.4745° |
| orbit number at epoch: | 51426 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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