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 26040.63748793 +.00000000 +00000-0 +10450-3 0 00000
2 07530 101.9973 52.5261 0012245 15.9548 97.0784 12.53695674 07
| Epoch (UTC): | 09 February 2026 15:17:58 |
| Eccentricity: | 0.0012245 |
| inclination: | 101.9973° |
| perigee height: | 1439 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 52.5261° |
| argument of perigee: | 15.9548° |
| revolutions per day: | 12.53695674 |
| mean anomaly at epoch: | 97.0784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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