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 42834U 17042K 25073.41917618 .00011081 00000-0 82991-3 0 9992
2 42834 97.3804 248.4415 0010330 187.7120 172.3948 15.02826660417782
| Epoch (UTC): | 14 March 2025 10:03:36 |
| Eccentricity: | 0.0010330 |
| inclination: | 97.3804° |
| perigee height: | 551 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 248.4415° |
| argument of perigee: | 187.7120° |
| revolutions per day: | 15.02826660 |
| mean anomaly at epoch: | 172.3948° |
| orbit number at epoch: | 41778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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