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 54255U 22155E 25322.53933227 .00033957 00000-0 77376-3 0 9994
2 54255 97.5980 88.7105 0006467 62.1656 298.0245 15.42840600167058
| Epoch (UTC): | 18 November 2025 12:56:38 |
| Eccentricity: | 0.0006467 |
| inclination: | 97.5980° |
| perigee height: | 433 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 88.7105° |
| argument of perigee: | 62.1656° |
| revolutions per day: | 15.42840600 |
| mean anomaly at epoch: | 298.0245° |
| orbit number at epoch: | 16705 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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