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 39133U 13015D 25137.45726365 .00007825 00000-0 36037-3 0 9999
2 39133 64.8700 105.4770 0030445 283.9379 75.8363 15.20550863664066
| Epoch (UTC): | 17 May 2025 10:58:27 |
| Eccentricity: | 0.0030445 |
| inclination: | 64.8700° |
| perigee height: | 483 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 105.4770° |
| argument of perigee: | 283.9379° |
| revolutions per day: | 15.20550863 |
| mean anomaly at epoch: | 75.8363° |
| orbit number at epoch: | 66406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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