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 23342U 94074A 25193.35369398 .00000664 00000-0 85084-4 0 9999
2 23342 97.6892 219.3198 0002153 99.0339 261.1119 14.84388411653506
| Epoch (UTC): | 12 July 2025 08:29:19 |
| Eccentricity: | 0.0002153 |
| inclination: | 97.6892° |
| perigee height: | 614 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 219.3198° |
| argument of perigee: | 99.0339° |
| revolutions per day: | 14.84388411 |
| mean anomaly at epoch: | 261.1119° |
| orbit number at epoch: | 65350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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