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 26053.64488102 +.00000000 +00000-0 +95502-5 0 00003
2 07530 101.9973 65.6727 0012113 351.1883 123.3630 12.53695981 04
| Epoch (UTC): | 22 February 2026 15:28:37 |
| Eccentricity: | 0.0012113 |
| inclination: | 101.9973° |
| perigee height: | 1440 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 65.6727° |
| argument of perigee: | 351.1883° |
| revolutions per day: | 12.53695981 |
| mean anomaly at epoch: | 123.3630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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