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 25174.32307467 .00000387 00000-0 82071-4 0 9990
2 29 48.3789 289.1718 0022338 165.0876 195.0701 14.78032208489143
| Epoch (UTC): | 23 June 2025 07:45:13 |
| Eccentricity: | 0.0022338 |
| inclination: | 48.3789° |
| perigee height: | 620 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 289.1718° |
| argument of perigee: | 165.0876° |
| revolutions per day: | 14.78032208 |
| mean anomaly at epoch: | 195.0701° |
| orbit number at epoch: | 48914 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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