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 25173.51184289 .00000386 00000-0 81962-4 0 9992
2 00029 48.3790 293.0226 0022310 161.5589 198.6138 14.78031188488918
| Epoch (UTC): | 22 June 2025 12:17:03 |
| Eccentricity: | 0.0022310 |
| inclination: | 48.3790° |
| perigee height: | 620 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 293.0226° |
| argument of perigee: | 161.5589° |
| revolutions per day: | 14.78031188 |
| mean anomaly at epoch: | 198.6138° |
| orbit number at epoch: | 48891 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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