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 13553U 82092B 25193.53397189 .00000300 00000-0 31166-4 0 9997
2 13553 82.5679 5.9890 0021054 21.9593 35.7328 14.86339890293258
| Epoch (UTC): | 12 July 2025 12:48:55 |
| Eccentricity: | 0.0021054 |
| inclination: | 82.5679° |
| perigee height: | 594 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 5.9890° |
| argument of perigee: | 21.9593° |
| revolutions per day: | 14.86339890 |
| mean anomaly at epoch: | 35.7328° |
| orbit number at epoch: | 29325 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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