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 is defined by the following mean orbital elements,
1 07547U 26150.52123816 +.00000000 +00000-0 +00000-0 0 00008
2 07547 3.6149 280.8938 0002330 194.7938 51.3971 1.00386447 04
| Epoch (UTC): | 30 May 2026 12:30:34 |
| Eccentricity: | 0.0002330 |
| inclination: | 3.6149° |
| perigee height: | 35745 km |
| apogee height: | 35764 km |
| right ascension of ascending node: | 280.8938° |
| argument of perigee: | 194.7938° |
| revolutions per day: | 1.00386447 |
| mean anomaly at epoch: | 51.3971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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