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 00029U 60002B 25082.85035343 .00003053 00000-0 44826-3 0 9995
2 00029 48.3791 3.3132 0022136 130.1044 230.1814 14.77782077475504
| Epoch (UTC): | 23 March 2025 20:24:30 |
| Eccentricity: | 0.0022136 |
| inclination: | 48.3791° |
| perigee height: | 621 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 3.3132° |
| argument of perigee: | 130.1044° |
| revolutions per day: | 14.77782077 |
| mean anomaly at epoch: | 230.1814° |
| orbit number at epoch: | 47550 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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