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 13121U 82027B 25194.80088677 .00004025 00000-0 16202-3 0 9997
2 13121 81.1912 319.2121 0009225 11.9903 348.1548 15.24608240362402
| Epoch (UTC): | 13 July 2025 19:13:16 |
| Eccentricity: | 0.0009225 |
| inclination: | 81.1912° |
| perigee height: | 485 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 319.2121° |
| argument of perigee: | 11.9903° |
| revolutions per day: | 15.24608240 |
| mean anomaly at epoch: | 348.1548° |
| orbit number at epoch: | 36240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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