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 07318U 74039A 25118.89064889 .00000002 00000-0 00000-0 0 9993
2 07318 2.9672 261.0695 0027769 326.2417 332.0511 1.01977686117775
| Epoch (UTC): | 28 April 2025 21:22:32 |
| Eccentricity: | 0.0027769 |
| inclination: | 2.9672° |
| perigee height: | 35199 km |
| apogee height: | 35430 km |
| right ascension of ascending node: | 261.0695° |
| argument of perigee: | 326.2417° |
| revolutions per day: | 1.01977686 |
| mean anomaly at epoch: | 332.0511° |
| orbit number at epoch: | 11777 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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