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 00979U 65004B 25197.77008018 .00000043 00000-0 81214-4 0 9992
2 00979 96.4046 210.7481 1137993 272.3663 74.7848 12.15399763674811
| Epoch (UTC): | 16 July 2025 18:28:54 |
| Eccentricity: | 0.1137993 |
| inclination: | 96.4046° |
| perigee height: | 703 km |
| apogee height: | 2522 km |
| right ascension of ascending node: | 210.7481° |
| argument of perigee: | 272.3663° |
| revolutions per day: | 12.15399763 |
| mean anomaly at epoch: | 74.7848° |
| orbit number at epoch: | 67481 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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