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 07434U 74071B 25131.78089741 .00000339 00000-0 12046-3 0 9994
2 07434 74.0452 312.0739 0021039 230.9057 129.0226 14.37980264650870
| Epoch (UTC): | 11 May 2025 18:44:29 |
| Eccentricity: | 0.0021039 |
| inclination: | 74.0452° |
| perigee height: | 750 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 312.0739° |
| argument of perigee: | 230.9057° |
| revolutions per day: | 14.37980264 |
| mean anomaly at epoch: | 129.0226° |
| orbit number at epoch: | 65087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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