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 07530U 26049.89501455 +.00000000 +00000-0 -44950-4 0 00003
2 07530 101.9973 61.8827 0012165 358.3557 119.0568 12.53695919 00
| Epoch (UTC): | 18 February 2026 21:28:49 |
| Eccentricity: | 0.0012165 |
| inclination: | 101.9973° |
| perigee height: | 1440 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 61.8827° |
| argument of perigee: | 358.3557° |
| revolutions per day: | 12.53695919 |
| mean anomaly at epoch: | 119.0568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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