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 38770U 12048N 25198.85676210 .00027947 00000-0 52670-3 0 9992
2 38770 64.6410 322.3977 0090883 267.6823 91.3906 15.43916670 66690
| Epoch (UTC): | 17 July 2025 20:33:44 |
| Eccentricity: | 0.0090883 |
| inclination: | 64.6410° |
| perigee height: | 372 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 322.3977° |
| argument of perigee: | 267.6823° |
| revolutions per day: | 15.43916670 |
| mean anomaly at epoch: | 91.3906° |
| orbit number at epoch: | 6669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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