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 31789U 07028A 25191.63090431 .00096977 10203-4 40718-3 0 9990
2 31789 64.4735 305.6610 0025516 302.8205 57.0494 15.85082712997822
| Epoch (UTC): | 10 July 2025 15:08:30 |
| Eccentricity: | 0.0025516 |
| inclination: | 64.4735° |
| perigee height: | 299 km |
| apogee height: | 333 km |
| right ascension of ascending node: | 305.6610° |
| argument of perigee: | 302.8205° |
| revolutions per day: | 15.85082712 |
| mean anomaly at epoch: | 57.0494° |
| orbit number at epoch: | 99782 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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